Presentación de PowerPointaero.us.es/adesign/Trabajos/Curso_2017_18/GIA/Grupo_03... · 2018-11-04 · Fracciones de peso 80000 80000 280 285.71 1º FL 79830,8 46301.86 261,9 304.81

Origen universitario

Emprendimiento

Compromiso social

NOSOTROS

ORGANIGRAMA

Estructuras

Paola Carmona

Juan Manuel Lora

Propulsioacuten

BeatrizArbona

Pablo Fernaacutendez

Jesuacutes Rodriacuteguez

Estabilidad

Ana Casares

Ana Retamal

Joseacute Mariacutea Ramiacuterez

Aerodinaacutemica

Rafael Feacutelix

Laura Garciacutea

Disentildeo y sistemas

Aacutelvaro Anega

Roberto Bustamante

Pedro Goacutemez-Coronado

iquestPor queacute

Servicio personalizado

Garantiacutea de calidad

Organizacioacuten

Facilidad de gestioacuten

DISENtildeO

EVOLUCIOacuteN DEL DISENtildeO DEL FL-18

DESCRIPCIOacuteN GEOMEacuteTRICA

Las cotas para cada una de las 3 vistas vienen indicadas en el informe

GENERAL

DESCRIPCIOacuteN GEOMEacuteTRICA DETALLADA

Fuselaje

DESCRIPCIOacuteN GEOMEacuteTRICA DETALLADAInterior del

fuselaje

DESCRIPCIOacuteN GEOMEacuteTRICA DETALLADAInterior de la cabina

Superficies hipersustentadoras

Tren de aterrizaje

Dimensiones

Altura fuselaje (Hf) 119m

Xn 088 m

Xm 112 m

Wheel BaseBatalla (B) 1031 m

Aacutengulo overturn 295ordm

Aacutengulo clearance 1739ordm

Wheel Track 369 m

DESCRIPCIOacuteN DE LOS SISTEMAS

Sistema de combustibleDepoacutesitos de combustibleSistema de control de vueloSistema hidraacuteulicoSistema antiincendiosSistema antihieloSistema eleacutectrico

ADECUACIOacuteN A LA CARGA DE PAGO

ARQUITECTURA INTERNA

AVANCES TECNOLOacuteGICOS Y POSIBLES MEJORAS

Avances tecnoloacutegicos

bull More ElectricAircraft

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

bull Materialescompuestos

Posibles mejoras

bull Superficie alar

bull Tren de aterrizaje

bull Almacenamiento retardante

bull Suelta retardante

ESTRUCTURAS

Estructuras

FLAM-AIR

Disentildeo y Sistemas

Propulsioacuten y Actuaciones

Aerodinaacutemica

Estabilidad

Caacutelculo de pesos Caacutelculo de esfuerzos Materiales empleados

ESTRUCTURAS ndash Evolucioacuten pesos

Evolucioacuten MTOW [kg] Wvaciacuteo [KG] Superficie [m2] WS

Fracciones de peso 80000 80000 280 28571

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

ESTRUCTURAS ndash Evolucioacuten de pesos

Fraccionesde peso

1ordm FL 2ordm FL 3ordm FL 1ordm MC Final MC

Evolucioacuten Pesos MTOW

Fracciones depeso

Evolucioacuten Superficie y WS Superficie[m]

WS [-]

ESTRUCTURAS ndash Comparativa con otros avionesCASA C-295 W Bombardier CL-415Grumman S-2T Turbine Tracker

Lockheed C-130

Wempty [Kg] MTOW [Kg] S [m2]

Grumman S-2T 8310 11860

CASA C-295W 11450

Bombardier CL-415 12882

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

ESTRUCTURAS ndash Factores lineales

Elementos Kg Peso total

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

Pesos globales Kg Peso total

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

ESTRUCTURAS ndash Meacutetodo Completo

Meacutetodo iquestQueacute iquestCoacutemo

Sadrey Estima pesos de los

elementos estructurales

Empleando ecuaciones parameacutetricas basadas e bull Relacioacuten peso-densidad media bull Evidencias experimentales bull Material empleado

GD Estima pesos de los

Empleando foacutermulas basadas en bull Datos histoacutericos bull Geometriacutea y caracteriacutesticas de

aeronave

Estima el peso de los elementos del avioacuten

en vaciacuteo y sus sistemas

Empleando tablas relativas al porcentaje sobr peso total de cada elemento o sistema

Torenbeek+GD Estima pesos de sistemas

Combinando ambos meacutetodos

Estructura 107494 2757

Refuerzos 384466 098

Sistemas 406007 1041

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Elementos estructurales Peso [kg] Peso Estructural

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Fuselaje 190705 1712

Tren 107264 963

Motores 378879 3402

Sistemas Peso [kg] Peso Sistemas

Control de vuelo 50943 1254

Hidraacuteulico 272982 672

Instrumentacioacuten 498639 1228

Electricidad 672618 1656

API + Oxiacutegeno 7697727 1895

APU 194987 480

Mobiliario 902749 2223

Equipaje 238866 588

ESTRUCTURAS ndash Centros de gravedad

Factores Lineales Meacutetodo Completo

Actuaciones Estabilidad

Evolucioacuten Centro de gravedad

Cdg respecto al morro

Inicial Despegue Subida 1 Subida 2 Crucero Descenso 1ordm DescargaViraje

2ordm DescargaViraje

Subida 3 Crucero 2 Descenso 2 Descenso 3 Aterrizaje+taxi

Kg RetardanteKg Fuel

Payload Fuel

ESTRUCTURAS ndash Cargas aerodinaacutemicas

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

Distribucioacuten de cortantes

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

Distribucioacuten de momento flector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Distribucioacuten de Torsores

ESTRUCTURAS ndash Cargas estructurales

Carrera de despegue Balance al frenado Remolque

Two and Three points Tail down landing One Wheel landingAterrizaje ndash 2 puntos Aterrizaje - 3 puntos Aterrizaje - 3 puntos

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Tail Down landing One ndash Wheel Landing

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Aterrizaje ndash 2 puntos Aterrizaje - 3 puntos Aterrizaje ndash 3 puntos

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Solo tren principal Tren de morro (NG) Tren principal(MG)

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Tren de morro (NG) Tren principal(MG)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

ESTRUCTURAS ndash Diagrama V_n

Misioacuten Primera Liacutenea

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Raacutefaga no restrictiva

Se cumple con RFP del cliente

ESTRUCTURAS ndash Material y Refuerzos

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

REDUCCIOacuteN DE MATERIAL

Fuselaje20

Tren de aterrizaje27

REFUERZOS

PROPULSIOacuteN Y ACTUACIONES

SELECCIOacuteN DE CARGA ALAR

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

ESTIMACIONES PRELIMINARES

MODELO DE REFERENCIAC-130H Hercules Configuracioacuten

sucia Configuracioacuten media

Configuracioacuten limpia

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

ESTUDIO PRELIMINAR POTENCIA PESO

Potencia disponible [kW] Potencia disponible [shp] MTOW [kg] PSLWTo [WN]

9133764 12248561 389966 23961

SELECCIOacuteN PLANTA DE POTENCIA

planta motora tipo turboheacutelice

Buacutesqueda de motores

Tipo de motor Potencia [shp]Consumo

[lb(hrmiddotshp)]Peso [lb]

Napier Eland NEl6 Mk504A

3500 ~ 1820

General Electric T64-GE-P4D-1

3400 048 1188

Europrop TP400-D6 (A400M)

11000 039 4035

Rolls-Royce Tyne RTy12 Mk101

5460 045 2219

Rolls-Royce Tyne RTY20 MK 21

6100 045 2203

bull Potencia total al nivel del mar por motor 5 460 shpbull Nuacutemero de motores 4bull Consumo a nivel del mar 045 119897119897119897119897

ℎ119903119903lowastℎ119901119901bull Peso por motor 10065 kg [total 40261 kg]bull Diaacutemetro de las heacutelices 427metros [dimensionadas del Fokker F-27]

Datos baacutesicos de la planta propulsora

Datos adicionales de la heacutelice

bull Nuacutemero de palas por heacutelice 4bull Torsioacuten de la pala en el 75 de la cuerda 15ordmbull Tipo de heacutelice heacutelice de paso fijobull Rendimiento moto-propulsivo 082

Dimensionado

Escalado 75 Escalado 60 [definitivo]Potencia por motor 4095 [shp] 3276 [shp]

Potencia total (4 motores) 16380 [shp] 13104 [shp]Peso por motor 754875 [kg] 6039 [kg]

Peso total (4 motores) 301950 [kg] 24156 [kg]Longitud del motor 25154 [m] 233508 [m]Diaacutemetro del motor 099698 [m] 092551 [m]

Diaacutemetro palas de la heacutelice 403125 [m] 38553 [m]

CONSUMO ESPECIacuteFICO

Misioacuten primera liacutenea

Misioacuten ferry

Despegue Subida Crucero-ida Crucero-vuelta Descenso05552355 06088772 07057481 07064883 10975105

Despegue Subida Crucero (max Alcance) Crucero (max Autonomiacutea) Descenso05046 05351 05455 05474 0949

POTENCIA REQUERIDA FRENTE A POTENCIA DISPONIBLE

MISIOacuteN DE PRIMERA LIacuteNEA

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

Velocidad minimiza CASM

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tramo de vuelo Consumo de combustible [kg]

Tiempo de vuelo [s]

Taxi [5000ft] 304166 540Despegue [5000ft] 102158 145112Subida 1[5000ft-6500ft] 289978 404287Subida 2 [6500ft-15000ft] 223955 3221448Crucero 1 [15000ft] 9350784 17781852Descenso 1 [15000ft-300ft] 778151 1016382Virajes [300ft] 316698 1164681Subida 3 [300ft-15000ft] 1401829 2125668Crucero 2 [15000ft] 8286857 19519787Descenso 2 [15000ft-6500ft] 303497 4553539Descenso 3 [6500ft-5000ft] 420671 6361806Aterrizaje [5000ft] 15155 250178Taxi [5000ft] 168981 300

MISIOacuteN DE FERRY

FUEL TOTAL

119934119934119943119943 = 78609125 kg

Velocidad minimiza combustible

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

Tramo de vuelo Consumo de combustible [kg] Tiempo de vuelo [s]

Taxi y despegue [5000ft] 327644 34973Subida 1[5000ft-6500ft] 8376 125635Subida 2 [6500ft-15000ft] 986291 1709673Crucero [20000ft] 7596697 43318422Descenso 1 [20000ft-6500ft]

711237 12658515

Descenso 2 [6500ft-5000ft] 33903 5557826Aterrizaje y taxi [5000ft] 184193 286516

RESERVA DE COMBUSTIBLE

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MISIOacuteN DE RESERVA

COMPARACIOacuteN MISIONES

Misioacuten primera liacutenea DESPEGUE ATERRIZAJEDistancia 15ordmC 4451247 [m] 6412728 [m]Distancia 35ordmC 4589844 [m] 6403518 [m]

Fuel 15ordmC 102158 [kg] 15155 [kg]Fuel 35ordmC 108713 [kg] 15794 [kg]

Misioacuten ferry DESPEGUE ATERRIZAJEDistancia 15ordmC 1725239 [m] 8325956 [m]Distancia 35ordmC 1733785 [m] 8327369 [m]

OPTIMIZACIOacuteN DE OPERACIONES

Optimizacioacuten CASM

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

CARGA DE PAGO- ALCANCE

Ra Rb Rc241248 [nm] 3334811 [nm] 4000127 [nm]446791 [km] 6176070 [km] 7408235 [km]

AERODINAacuteMICA

Problema 2D Eleccioacuten de perfiles

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

Iteracioacuten 119930119930119955119955119955119955119943119943 AR b 119914119914119915119915120782120782 120630120630119930119930119930119930119930119930119930119930119930119930 119914119914119930119930119914119914119915119915 119950119950119898119950119950

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

ARdarr 119890119890 uarr

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

Dispositivos hipersustentadores

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

Meacutetodo numeacuterico

Meacutetodo mixto00272578340

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

CG maacutes atrasado

CG maacutes adelantado

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

TRIMADO LONGITUDINAL

Misioacuten de Primera Liacutenea1ordm ITERACIOacuteN 2ordm ITERACIOacuteN

ESTABILIDAD ESTAacuteTICA

ESTABILIDAD

ESTABILIDAD ESTAacuteTICATRIMADO LONGITUDINAL

3ordm ITERACIOacuteN

ESTABILIDAD

ESTABILIDAD ESTAacuteTICATRIMADO LONGITUDINAL3ordm ITERACIOacuteN

ESTABILIDAD

Misioacuten de Ferry

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

TRIMADO LATERAL-DIRECCIONAL

ESTABILIDAD

ITERACIOacuteN 1ITERACIOacuteN 2ITERACIOacuteN 3ITERACIOacuteN 4

FALLO DE MOTOR Y RESBALAMIENTO

ESTABILIDAD

MOTOR SIN RESBALAMIENTOMOTOR CON RESBALAMIENTO

ESTABILIDAD

ITERACIOacuteN 1ITERACIOacuteN 2ITERACIOacuteN 3

ESTABILIZADOR VERTICAL

ESTABILIDAD

ESTABILIZADOR HORIZONTAL

ITERACIOacuteN 1ITERACIOacuteN 2

ESTABILIDAD

ALERONES

ALERONES MISIOacuteN PRIMERA LIacuteNEAALERONES FERRY

ESTABILIDAD

ESTABILIDAD DINAacuteMICA LONGITUDINALModo w [rads] [s] T [s]

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

COMPORTAMIENTO DINAacuteMICO LONGITUDINAL

ESTABILIDAD

ESTABILIDAD DINAacuteMICA LATERAL-DIRECCIONALModo w [rads] [s] T [s] [s]

Balanceo holandeacutes

17072 39959 36996 010159

Espiral 8163824

Convergencia en balance

014647

COMPORTAMIENTO DINAacuteMICO LATERAL-DIRECCIONAL

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

Gracias por pensar en

NUESTRO PRODUCTO

Nuacutemero de diapositiva 1

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Aterrizaje + taxi

953217

Depoacutesito Alas

Depoacutesito

Voluacutemenes [m3]

ME []

Aeronave en vaciacuteo

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

1ordm Descarga Viraje

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Tren de morro (NG)

Tren principal(MG)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Solo tren principal

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Aterrizaje ndash 2 puntos

Aterrizaje - 3 puntos

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Tail Down landing

One ndash Wheel Landing

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

Instrumentacioacuten

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Elementos estructurales

Peso [kg]

Peso Estructural

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Estima pesos de los elementos estructurales

Empleando ecuaciones parameacutetricas basadas en

middot Relacioacuten peso-densidad media

middot Evidencias experimentales

middot Material empleado

Empleando foacutermulas basadas en

middot Datos histoacutericos

middot Geometriacutea y caracteriacutesticas de la aeronave

Estima el peso de los elementos del avioacuten en vaciacuteo y sus sistemas

Empleando tablas relativas al porcentaje sobre el peso total de cada elemento o sistema

Torenbeek+GD

Estima pesos de sistemas

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Bombardier CL-415

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Wvaciacuteo [KG]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

ORGANIGRAMA

Estructuras

Paola Carmona

Juan Manuel Lora

Propulsioacuten

BeatrizArbona

Pablo Fernaacutendez

Jesuacutes Rodriacuteguez

Estabilidad

Ana Casares

Ana Retamal

Joseacute Mariacutea Ramiacuterez

Aerodinaacutemica

Rafael Feacutelix

Laura Garciacutea

Disentildeo y sistemas

Aacutelvaro Anega

Roberto Bustamante

Pedro Goacutemez-Coronado

iquestPor queacute

Organizacioacuten

DISENtildeO

GENERAL

Fuselaje

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

iquestPor queacute

Organizacioacuten

DISENtildeO

GENERAL

Fuselaje

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

DISENtildeO

GENERAL

Fuselaje

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

GENERAL

Fuselaje

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

GENERAL

Fuselaje

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Fuselaje

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

fuselaje

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Tren de aterrizaje

Dimensiones

Xn 088 m

Xm 112 m

Wheel Track 369 m

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

bull Fly by Wire

bull FADEC

bull CPIOMs y AFDX

Posibles mejoras

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

ESTRUCTURAS

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Estructuras

FLAM-AIR

Aerodinaacutemica

Estabilidad

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

5125 4953

1ordm FL 798308 4630186 2619 30481

2ordm FL 558945 298618 18235 306523

3ordm FL 534188 278873 141306 37801

1ordm MC 420417 180381 141306 297517

Final MC 389965 15194 141306 275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Evolucioacuten

MTOW [kg]

Superficie [m2]

Fracciones de peso

1ordm FL

798308

4630186

2ordm FL

558945

298618

306523

3ordm FL

534188

278873

141306

1ordm MC

420417

180381

141306

297517

Final MC

389965

141306

275978

Fraccionesde peso

Fracciones depeso

WS [-]

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Lockheed C-130

Grumman S-2T 8310 11860

CASA C-295W 11450

Lockheed P-2V 15819 29076 922

Flam-Air FL-18 15194 389965 1413

Lockheed C-130H 34400 70300 1621

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Wempty [Kg]

MTOW [Kg]

S [m2]

Grumman S-2T

CASA C-295W

Lockheed P-2V

Flam-Air FL-18

15194

389965

1413

Lockheed C-130H

Ala 617686 221493

Htp 540 1936

Vtp 41843 15

Fuselaje 413986 148449

Tren 229702 8236

Motores 523393 187681

We 278873 522051

Payload 204116 380105

Wcrew 200 03744

Wfuel 491987 921

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

aeronave

Crew 200 051

Payload 204116 5234

Fuel 319093 818

Ala 373463 3354

HTP 350196 314

VTP 280602 252

Tren 107264 963

Motores 378879 3402

APU 194987 480

Equipaje 238866 588

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Sistemas

Peso [kg]

Peso Sistemas

Control de vuelo

Hidraacuteulico

272982

498639

Electricidad

672618

API + Oxiacutegeno

7697727

194987

Mobiliario

902749

Equipaje

238866

Peso [kg]

373463

350196

280602

Fuselaje

190705

107264

Motores

378879

Pesos globales

Peso total

Estructura

107494

Refuerzos

384466

Sistemas

406007

Payload

204116

319093

Meacutetodo

iquestQueacute

iquestCoacutemo

Sadrey

Torenbeek+GD

Payload Fuel

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Elementos

S 4307 m2

MTOW 389965 kg

n_max 25

q_max 122 MPa

cm -003421

020000400006000080000

100000120000140000160000

1 2 3 4 5 6 7 8 9 10Fuer

Sector

0200400600800

100012001400

1 2 3 4 5 6 7 8 9 10Mom

Sector

-6000-5000-4000-3000-2000-1000

1 2 3 4 5 6 7 8 9 10

Sector

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Elementos

4307 m2

389965 kg

122 MPa

-003421

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119 32463 38631 3694402 282286 335921 1553434 84686 10077

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856 5069579 6032799 44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119 1069665 12729 3690361 93014 110687 1561516 27904 33206

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034 1560827 1857384 1612871 1290297 1535453 676326 541061 643862

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688 599267 269448 6681815 94348 1122741

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1578688

599267

269448

6681815

1122741

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

1951034

1560827

1857384

1612871

1290297

1535453

676326

541061

643862

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG (N)

Flector NG (Nm)

4471119

1069665

3690361

110687

1561516

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

44422856

5069579

6032799

44711193

Axial MG(N)

Cortante MG (N)

Flector MG (Nm)

Axial MG (N)

Cortante MG (N)

Flector MG (Nm)

Axial NG (N)

Cortante NG(N)

Flector NG (Nm)

4471119

3694402

282286

335921

1553434

Misioacuten Ferry

Factores de Carga

N max 25

N min -1

N lim 375

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Factores de Carga

Compuestos50

Aluminio20

Acero8

Titanio14

Otros8

COMPOSICIOacuteN

Fuselaje15

Tren de aterrizaje5

Motores18

Fuselaje20

REFUERZOS

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Superficie alar

119904119904119908119908119908119908119908119908119904119904119903119903119908119908119903119903

PROPULSIOacuteN

119862119862119862119862119900119900 0021 0018 0014

CARGA ALAR

119882119882119878119878 = 275978

1198961198961198961198961198981198982

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

9133764 12248561 389966 23961

3500 ~ 1820

3400 048 1188

11000 039 4035

5460 045 2219

6100 045 2203

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Dimensionado

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Misioacuten ferry

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

FUEL TOTAL

119934119934119943119943 = 120784120784120784120784120784120784120784120784120790120790120790120790120790120790 119844119844119844119844

119881119881119900119900119901119901119908119908 = 1485522 frasl119898119898 119904119904

ACTUACIONES

Tiempo de vuelo [s]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

FUEL TOTAL

119934119934119943119943 = 78609125 kg

119881119881119900119900119901119901119908119908 = 852648 frasl119898119898 119904119904

711237 12658515

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

119934119934119943119943 = 120788120788120782120782120784120784120782120782120790120790120782FUEL TOTAL

119934119934119943119943 = 120790120790120784120784120790120790120784120784120784120784120784120784120790120790 119844119844119844119844

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

MACH CASM0415 99971

04345 98851045 9843046 98344

0481 9864704965 99266

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

642-215

653-218

644-221

652-215

63-209

64-210

Iteracioacuten 1

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

643-418

653-618

644-421

633-418

65-410

Iteracioacuten 2

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

633-418

119862119862119897119897119898119898119898119898119898 = 2007 119864119864119898119898119898119898119898 = 150997

α119878119878119878119878119878119878119878119878119878119878 = 21119862119862119889119889119898119898119898119898119898 = 000425

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

119862119862119897119897119898119898119898119898119898 = 2096 119864119864119898119898119898119898119898 = 160258

α119878119878119878119878119878119878119878119878119878119878 = 22839119862119862119889119889119898119898119898119898119898 = 00048178

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Problema 3D

AERODINAacuteMICA

119914119914119930119930119950119950119898119950119950 119914119914119930119930120782120782 119914119914119930119930120630120630

1 182426 1059 4395 0005747030 195 366129 1691182 01410579 56638

2 (CP) 182426 1059 4395 0004982486 235 441055 1942788 02995903 5972

3 141306 9 3566 0006659609 25 40967376 1937877 0291737 54599

final 141306 9 3566 0004744923 25 40686795 19506650 0291715 55098

119890119890 = 0958605541

iquestWinglets NO

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

119890119890119898119898119898119898119898 120582120582 = 05593 119890119890 = 0958605541

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Problema 3D

AERODINAacuteMICA

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Estabilizadores

AERODINAacuteMICA

FOS 35378 554 14 0005045093 0 0 48248

3 20 5 10 0005045093 0 0 48248

Final (darr 119875119875) 20 5 10 0005019599 0 0 46442

FOS 152 105 4 0 0 0 48248

3 154974 15 48214 0002134323 0 0 50681

Final (darr 119875119875) 154974 15 48214 0003893203 0 0 19078

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Estabilizadores

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Avioacuten completo

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

3 iteraciones

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

1198621198621198631198630 = 120782120782 120782120782120784120784120783120783120783120783120787120787120790120790120790120790120782120782120787120787120784120784

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

AERODINAacuteMICA

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

ESTABILIDAD

CENTROS DE GRAVEDAD

ME gt 0 CG = 10144m

119950119950119940119940119940119940 = 119925119925120782120782 minus119914119914119924119924120782120782 + 119914119914119924119924120633120633119955119955

120633120633119955119955119950119950119950119950119950119950

119914119914119949119949120630120630120630120630119960119960119950119950119950119950119950119950= 120784120784120783120783120790120790120790120790 CG = 8903m ME = 314

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

905

ME []

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

1027

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

Evolucioacuten

ME []

Inicial

951055

Despegue

Subida 1

Subida 2

Crucero

Descenso

Subida 3

Crucero 2

939814

Descenso 2

Descenso 3

PL_f

PL_Nf

NPL_f

NPL_Nf

Posicioacuten [m]

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

ESTABILIDAD

119881119881119908119908 = 791 119881119881119867119867119878119878119867119867 = 209 120782

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

Depoacutesito

ME []

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

953217

Posicioacuten [m]

Evolucioacuten

ME []

Inicial

953217

Despegue

953217

Subida

953217

Crucero

953217

Descenso

953217

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

ALERONES

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

Corto periodo

111775 0062 Inf 1

Fugoide 010388 15181 673323 043943

Modo K1 K2 K3 K4

-111775 62764 -004569+0093316i -004569-0093316i

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

ESTABILIDAD

17072 39959 36996 010159

Espiral 8163824

014647

Modo K1 K2 K3 K4 K5

0 -47314 -000084887 -017343+16984i -017343+16984i

NUESTRO PRODUCTO

[]	[]

351	0993	00373	-0342	-0941	605	0426	0317

[]	[]

-0152	224	00359	-0369	-0943	605	0426	0317

[]	[]

229	721	0136	-0418	-0947

[]	[]

351	0993	00373	-0342	-0941	605	0426	0317

[]	[]

-0152	224	00359	-0369	-0943	605	0426	0317

Evolucioacuten	[m]	ME []

Inicial	953217	154

Despegue	953217	154

Subida	953217	154

Crucero	953217	154

Descenso	953217	154

Aterrizaje + taxi	953217	154

	[m]	ME []

*PL_f*	9511	156

*PL_Nf*	9696	11

*NPL_f*	9091	259

*NPL_Nf*	9434	174

Factores de Carga

N max		25

N min		-1

N lim		375

Raacutefaga no restrictiva

Se cumple con RFP del cliente

Aterrizaje ndash 2 puntos	Aterrizaje - 3 puntos	Aterrizaje ndash 3 puntos

Axial MG(N)	Cortante MG (N)	Flector MG (Nm)	Axial MG (N)	Cortante MG (N)	Flector MG (Nm)	Axial NG (N)	Cortante NG (N)	Flector NG (Nm)

4471119	1069665	12729	3690361	93014	110687	1561516	27904	33206

Elementos

S		4307 m2

MTOW		389965 kg

n_max		25

FS		15

q_max		122 MPa

cm		-003421

		Posicioacuten [m]

		1015

		905

		2130

		Posicioacuten [m]

		1015

		905

		2130

	[m]	ME []

*PL_f*	9532	169

*PL_Nf*	9745	115

*NPL_f*	9167	261

*NPL_Nf*	9467	185

		Posicioacuten [m]

		992

		905

		2130

		1027

Documents

Presentación de PowerPointaero.us.es/adesign/Trabajos/Curso_2017_18/GIA/Grupo_03... · 2018-11-04 · Fracciones de peso 80000 80000 280 285.71 1º FL 79830,8 46301.86 261,9 304.81