flexo_compresion_v16

programa$=" flexo_compresion_v16" '8-2-13 2571

' #1 = ventana de dialogo principal (cierra todas ventanas)

' #t = pantalla de texto (salida de los calculos)

' #dat1 = pantalla de texto de salida de los datos

' #d = canal de entrada de los datos

' #5 = ventana de texto (entrada de la ayuda)

' #6 = canal de entrada del fichero de ayuda

' #g = ventada grafica de dibujo del esquema dela estructura

'....................................................................

nomainwin

dim properties(12), tipo$(15)

call configuracion

pi=4*atn(1) : r.g=360/(2*pi) : g.r=1/r.g : g$="SysGraph\"

noti$="Hola ";Usuario$;", soy el programa, lo siento,";chr$(10);_

"no puedo hacer nada si no";chr$(10);"buscas antes algun fichero."

UpperLeftX = 1 :WindowWidth = 455

UpperLeftY = 1 :WindowHeight =DisplayHeight*0.95

dim c$(5)

c$(1)="blue" :c$(2)="green":c$(3)="cyan":c$(4)="yellow":c$(5)=" white"

TextboxColor$=c$(3)

textbox #1.x1 , 3, 8,350,40

bmpbutton #1.dir,g$+"a.martinez4.bmp", [about],UL,360, 9

bmpbutton #1.buscar,g$;"lupa.bmp" , [buscar],UL, 33,48

bmpbutton #1.DAT ,g$;"RTANK2.bmp" , [AYUDA],UL,213,50

bmpbutton #1.con ,g$;"construction.bmp",[con],UL,280,50

TextboxColor$= c$(4) : textbox #1.pp$ , 3, 86,353,22

TextboxColor$= c$(3) : textbox #1.x3 , 3,110,152,40

TextboxColor$= c$(2) : textbox #1.L , 3,150, 34,20 'b base

textbox #1.H , 41,150, 34,20 'h Altura

textbox #1.p , 81,150, 34,20 'bw en secciones T

textbox #1.t ,121,150, 34,20 'hf en secciones T

TextboxColor$= c$(3) : textbox #1.x5 , 3,172, 35,20 'tipo

textbox #1.x6 , 41,172,112,20 'NOMBRE

textbox #1.Ndd , 3,216, 44,20 'Nd

textbox #1.x13 , 50,216, 44,20 'Mxd

textbox #1.Myd , 98,216, 44,20 'Myd

textbox #1.x14 , 3,256, 34,20

textbox #1.x15 , 41,256, 34,20

textbox #1.x16 , 81,256, 34,20

textbox #1.x17 ,121,256, 34,20

textbox #1.x18 , 56,306, 85,40 'ARMADOS

textbox #1.x19 , 2,346, 50,20 'COM

textbox #1.x20 , 2,366, 50,20 'TRAC 1

textbox #1.x21 , 2,386, 50,20 'TRAC 2

textbox #1.x9 ,163,199,195,43 'Unidades de ENTRADA

textbox #1.x10 ,163,270,195,20 'Unidades de SALIDA

textbox #1.vista,274,365, 83,20

TextboxColor$= c$(2)

textbox #1.tipo , 3,194, 35,20

textbox #1.nombre,41,194,112,20

textbox #1.Nd , 3,236, 44,20

textbox #1.Md ,50,236, 44,20

textbox #1.myd ,98,236, 44,20

textbox #1.re , 3,276, 34,20

textbox #1.ch ,41,276, 34,20 'coef seg hormigon

textbox #1.ca ,81,276, 34,20 'coef seg acero

textbox #1.cf ,121,276, 34,20 'coef seg fuerzas

textbox #1.nC , 56,346, 60,20 'nº barras compresion

textbox #1.dC ,120,346, 20,20 'diam " "

textbox #1.nT , 56,366, 40,20 'nº barras traccion nivel 1

textbox #1.dT ,100,366, 40,20 'diam " " "

textbox #1.nT2 , 56,386, 40,20 'nº barras traccion nivel 2

textbox #1.dT2 ,100,386, 40,20 'diam " " "

bmpbutton #1.port ,g$;"1325.bmp",[cerchas],UL,163,110

textbox #1.UeF ,185,245, 40, 20

textbox #1.UeM ,230,245, 40, 20

textbox #1.UeL ,275,245, 40, 20

statictext #1,"Momentos" ,160,293, 55, 20

textbox #1.UsM ,214,293, 40, 20

button #1.mT, "mT" ,[mT] ,UL,275,293, 35, 20

button #1.mkN,"mkN",[mkN],UL,322,293, 35, 20

statictext #1,"Cargas" ,160,315, 55, 20

textbox #1.UsF ,214,315, 40, 20

button #1.cm, "kN",[kN], UL,275,315, 25, 20

button #1.T , "T" ,[T] , UL,305,315, 25, 20

button #1.cm, "kL",[kL], UL,335,315, 25, 20

statictext #1,"Longitud" ,160,340, 55, 20

textbox #1.UsL ,214,340, 40, 20

button #1.cm, "cm",[cm], UL,275,340, 25, 20

button #1.m , "m" ,[m] , UL,305,340, 25, 20

button #1.in, "pu",[pu], UL,335,340, 25, 20

bmpbutton #1.calcular,g$;"434.bmp",[plot],UL,165,365

statictext #1, "Nº" ,165,430, 25,20

textbox #1.num ,190,430, 35,20

bmpbutton #1.marcar, g$;"marcar.bmp",[seccion.elegida],UL,240,430

button #1.escaf ,"Scala" ,[escala] ,UL,274,387, 40,20

textbox #1.esca ,274,409, 40,20

button #1.esca1 ,"+" ,[escala1],UL,276,430, 16,20

button #1.esca2 ,"-" ,[escala2],UL,296,430, 16,20

ttto=10

button #1.texto ,"Texto" , [textos],UL,317,387, 40,20

textbox #1.tex5 ,317,409, 40,20

button #1.tex1 ,"+" ,[text1] ,UL,318,430, 16,20

button #1.tex2 ,"-" ,[texto2] ,UL,338,430, 16,20

TextboxColor$= c$(3) : textbox #1.x11 ,155,486,110,20

textbox #1.x12 ,275,486, 78,20


statictext #1," r1 r2 r3" ,155,506,260,20

textbox #1.r1 ,152,526, 33,20

button #1.r11 ,"+" ,[gir.r11],UL,152,546, 16,20

button #1.r12 ,"-" ,[gir.r12],UL,169,546, 16,20

textbox #1.r2 ,192,526, 33,20

button #1.r21 ,"+" ,[gir.r21],UL,192,546, 16,20

button #1.r22 ,"-" ,[gir.r22],UL,209,546, 16,20

textbox #1.r3 ,232,526, 33,20

button #1.r31 ,"+" ,[gir.r31],UL,232,546, 16,20

button #1.r32 ,"-" ,[gir.r32],UL,249,546, 16,20

textbox #1.mx ,272,526, 38,20

bmpbutton #1.mxizq,g$;"Fizqui.bmp",[des.izq],UL ,274,548

bmpbutton #1.mxder,g$;"Fderec.bmp",[des.der],UL ,292,548

textbox #1.my ,315,526, 38,20

bmpbutton #1.myarr,g$;"Farrib.bmp",[des.arr],UL ,316,548

bmpbutton #1.myaba,g$;"Fabajo.bmp",[des.aba],UL ,334,546

textbox #1.mz ,365,526, 72,20

bmpbutton #1.mzmay,g$;"Zoom_out.bmp",[des.may],UL,366,548

bmpbutton #1.mzmen,g$;"Zoom_in.bmp" ,[des.men],UL,402,548

textbox #1.kk ,152,566, 33,20

button #1.kkma ,"+" ,[kk.ma],UL,152,590, 16,20

button #1.kkme ,"-" ,[kk.me],UL,169,590, 16,20

' button #1.curva,"RIGIDA 3D" ,[PortTipo3D],UL, 3,506,120,25

' button #1.r3D,"SECCION T" ,[Seccion.T],UL, 3,536,120,25

button #1.ras,"SECCIONES",[Flexion.Simple],UL, 3,545,100,20


textbox #1.hor ,3,570,52,20

textbox #1.ace ,3,595,52,20


textbox #1.e ,57,570,50,20 'fc$

textbox #1.pe ,57,595,50,20 'fy$


textbox #1.horu ,107,570,45,20 'UeT$

textbox #1.aceu ,107,595,45,20 'UeT$

'button #1.res,"Nueva perspectiva",[des],UL,232,566,120,25

bmpbutton #1.ros,g$;"DISKBTTN.bmp",[guardar.parametros],UL,272,590


bmpbutton #1.datos,g$;"SAVE2.bmp",[escribir.dat1],UL, 135,60

graphicbox #1.dor ,362,130 ,81,323 'helice2

graphicbox #1.dar , 3,217,150,330 'cielo

'----------------------------------------

ForegroundColor$ = "blue" ' c$(5)

open programa$ for dialog as #1

#1 "font arial 10 "

#1 "trapclose [fin]"

a$="!font arial 9 bold"

#1.x1 "H.A. 2013 - FLEXION Y COMPRESION"+chr$(13)+chr$(10)+_

"SECCIONES POLIGONALES" :#1.x1 ,"!Disable":#1.x1 "!font arial 9 17 bold"

#1.x5 "Nº" :#1.x5 ,"!Disable":#1.x5 "!font arial 8 "

#1.x6 "NOMBRE" :#1.x6 ,"!Disable":#1.x6 a$

#1.x9 "Unidades de ENTRADA" +chr$(13)+chr$(10)+_

"Cargas Momentos Long " :#1.x9 ,"!Disable":#1.x9 "!font arial 10 bold"

#1.x10 "Unidades de SALIDA" :#1.x10 ,"!Disable":#1.x10 "!font arial 10 bold"

#1.x11 " giros" :#1.x11 ,"!Disable"

#1.x12 "movimiento" :#1.x12 ,"!Disable"

#1.vista " VISTAS 2D" :#1.vista,"!Disable"

#1.x18 " ARMADOS"+chr$(13)+chr$(10)+" n d(mm)"' Codigo

#1.x18,"!Disable":#1.x18 "!font arial 6 15"

#1.x19 "COMP" :#1.x19,"!Disable"

#1.x20 "TRA.1":#1.x20,"!Disable"

#1.x21 "TRA.2":#1.x21,"!Disable"

#1.Ndd " Nd" :#1.Ndd,"!Disable": #1.Ndd a$

#1.x13 " Mxd" :#1.x13,"!Disable": #1.x13 a$

#1.Myd " Myd" :#1.Myd,"!Disable": #1.Myd a$

#1.x14 "rec" :#1.x14,"!Disable": #1.x14 a$

#1.x15 "cSh" :#1.x15,"!Disable": #1.x15 a$

#1.x16 "cSa" :#1.x16,"!Disable": #1.x16 a$

#1.x17 "cSf" :#1.x17,"!Disable": #1.x17 a$

#1.hor "HORMI":#1.hor,"!Disable": #1.hor a$

#1.ace "ACERO":#1.ace,"!Disable": #1.ace a$

'............................................................

Open g$+"a.martinez4.bmp" for Input as #F '

bitmapInfo$ = Input$(#F,LOF(#F)) '

Close #F '

bfType$ = Mid$(bitmapInfo$, 1, 2) 'Bitmap File Header '

bfSize = Value(Mid$(bitmapInfo$, 3, 4)) '

if bfSize<>24454 then notice "Repair dll sector 093XF45" : goto [fin] '

'...................................................................

loadbmp "c",g$;"helice2.bmp" :#1.dor "drawbmp c 0 0" '

loadbmp "c", g$;"cielo.bmp" :#1.dar "drawbmp c 0 0" '

#1.dar "flush" :#1.dor "flush" '

wait '

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

Function Value(x$) '

Select Case Len(x$) '

Case 1 '

Value = Asc(x$) '

Case 2 '

Value= Asc(Mid$(x$,1,1)) '

Value=Value+(Asc(Mid$(x$,2,1))*256)'

Case 3 '


Value=Value+(Asc(Mid$(x$,2,1))*256) '


Case 4 '



Value=Value+(Asc(Mid$(x$,3,1))*256^2) '


End Select '

End Function '

'---------------------------------------------------------

[guardar.datos] '

if fileName$="" then notice noti$:wait '

datos=1 : gosub [datos] :datos=0 '

wait '

'kkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkkk

[guardar.parametros] '


#dat1 "Parametros perspectiva" '

#dat1 "r1, ";r1;", r2, ";r2;", r3, ";r3;", mx, ";mx;_ '

", my, ";my;", mz, ";mz;", kk, ";kk;", escala, ";escala '

wait '

'-------------------------------------------------------------------

[kk.ma] kk=kk+1 :#1.kk kk :#1.kk,"!contents? kk" :wait

[kk.me] kk=kk-1 :#1.kk kk :#1.kk,"!contents? kk" :wait

[des.der] mx=mx-kk :#1.mx mx :gosub [des] :wait

[des.izq] mx=mx+kk :#1.mx mx :gosub [des] :wait

[des.arr] my=my-kk :#1.my my :gosub [des] :wait

[des.aba] my=my+kk :#1.my my :gosub [des] :wait

[des.may] mz=mz-5*kk:#1.mz mz :gosub [des] :wait

[des.men] mz=mz+5*kk:#1.mz mz :gosub [des] :wait

[gir.r11] r1=r1+kk :#1.r1 r1 :gosub [des] :wait

[gir.r12] r1=r1-kk :#1.r1 r1 :gosub [des] :wait





[escala] #1.esca, "!contents? escala"

planta=1 : #g "cls" :gosub [planta.alzado] :wait

[escala1] if escala<0 then escala=0

escala=escala+1: #1.esca escala


[escala2] if escala>0 then escala=0

escala=escala-1: #1.esca escala


[textos] #1.tex5, "!contents? ttto"

planta=1 :gosub [planta.alzado] :wait

[text1] if texto<0 then texto=0

ttto=ttto+1:#1.tex5 ttto


[texto2] if texto>0 then texto=0

ttto=ttto-1:#1.tex5 ttto


'---------------------------------------------------------

'coeficientes de salida

[cm] CsL$="cm": #1.UsL CsL$: wait

[m] CsL$="m" : #1.UsL CsL$: wait

[pu] CsL$="pu": #1.UsL CsL$: wait

[kN] CsF$="kN": #1.UsF CsF$: wait

[T] CsF$="T" : #1.UsF CsF$: wait

[kL] CsF$="kL": #1.UsF CsF$: wait

[mT] CsM$="mT": #1.UsM CsM$: wait

[mkN] CsM$="mkN":#1.UsM CsM$: wait

'-----------------------------------------------

[buscar] '

filedialog "Listar ficheros", "*.dat", fileName$ '

if fileName$<>"" then '

pp$= fileName$ '

#1.pp$ fileName$ '

call abrirdat '

open fileName$ for input as #datos2 '

'---------------------------------- '

t$="": line input #datos2, t$ :#dat1 t$ '

while eof(#datos2)=0 '

line input #datos2,t$ '

if t$<>"" then filas=filas+1 :#dat1 t$ '

wend '

close #datos2 '

'----------- '

if escala=0 then escala=1 :ttto=10 '

if kk=0 then kk=1 '

else '

notice noti$ '

end if '

wait '

'......................................

[seccion.elegida] '


open fileName$ for input as #datos2 '

#1.num,"!contents? numero" '

if numero>filas then numero=filas '

for n=1 to numero+1: line input #datos2,t$: next '

gosub [cabecera] '

gosub [datos.iniciales] '

call configuracion '

gosub [datos.pantalla] '

close #datos2 '

wait '

'.............................................................

[datos.pantalla] 'situa los datos desde el .dat en la pantalla izquierda

#1.r1 r1: #1.r2 r2 :#1.r3 r3:#1.mx mx:#1.my my:#1.mz mz

#1.kk kk: #1.esca escala:#1.L b :#1.H h :#1.p bw:#1.t hf

#1.e fc$ : #1.pe fy$ : #1.tipo tipo :#1.nombre nombre$

#1.tex5 ttto :#1.Md Md:#1.myd Myd:#1.Nd Nd:#1.re rec:#1.ch ch:#1.ca ca:#1.cf cf

#1.nC nC :#1.dC dC:#1.nT nT :#1.dT dT:#1.UeF UeF$:#1.UeM UeM$: #1.UeL UeL$

if UeT$="k" then UeT$="kg/cm2"

#1.horu UeT$ :#1.horu,"!Disable" :#1.horu "!font arial 7 bold"

#1.aceu UeT$ :#1.aceu,"!Disable" :#1.aceu "!font arial 7 bold"

return

'------------------------------------------------------------

[escalas]

a$=", "+t$ : ndc=len(a$)+2 :m=0

dim carac$(ndc)

dim dato(17)

For n=1 to ndc

carac$(n)=mid$(a$,n,1)

if carac$(n) ="," then m=m+1

if carac$(n-1)=" " then pepe=1

if pepe =1 then caracter$=caracter$+carac$(n)

if carac$(n) ="," then pepe=0

dato(m)=val(caracter$)

if carac$(n) ="," then caracter$=""

next n

ndd=m

r1=dato(2) :r2=dato(4) :r3=dato(6):mx=dato(8):my=dato(10)

mz=dato(12):kk=dato(14):escala=dato(16)

m=0

return

'........................................................................

[datos.iniciales] 'lee datos del fichero de texto *.dat

' nombre nº Fue UeF Md UeM rec UeL nC dC nT dT b h bw hf '

' FS_R_D01 1 0 kN 4.12 mT 4 cm 0 10 0 16 40 25 0 0 '

fck=0:fyk=0 :bw=0:hf=0 :desplaza=0 :COdA$="" '

a$=" "+t$+" " : ndc=len(a$)+2 : m=0 '

dim dato$(41) '

dim carac$(ndc) '

For n=1 to ndc '

carac$(n)=mid$(a$,n,1) '

if carac$(n)<>" " and carac$(n-1)= " " then m=m+1 '

if carac$(n)<>" " then pepe=1 '

if carac$(n) =" " and carac$(n-1)<>" " then pepe=0 '

if pepe =1 then caracter$=caracter$+carac$(n):dato$(m)=caracter$ '

if pepe =0 then caracter$="" '

next n '

'...............................................................................'

ndd=m : m=0 '

nombre$=dato$(1) :tipo=val(dato$(2)):fc$=dato$(3) :fy$=dato$(4):UeT1$=dato$(5)'

Nd =val(dato$(6)):UeF$=dato$(7) :Md=val(dato$(8)):Myd=val(dato$(9)) '

UeM$=dato$(10) :rec=val(dato$(11)):UeL$=dato$(12) :nC=val(dato$(13))

dC=val(dato$(14))

if len(dato$(13))>2 then 'secciones poligonales '

for n=1 to 2*len(dato$(13)) 'coordenadas de vertices '

if n mod 2 =1 then x((n+1)/2)=val(dato$(14+n)) '

if n mod 2 =0 then y(n/2) =val(dato$(14+n)) '

next '

end if '

if len(dato$(13))<3 then 'secciones rectangulares o T '

nT=val(dato$(15)):dT=val(dato$(16)) '

b =val(dato$(17)):h =val(dato$(18)):bw=val(dato$(19)):hf=val(dato$(20)) '

end if '

gosub [cabecera] '

UeT$=UeT1$ '

if fc$="0" then fc$=str$(fck.con) : fy$=str$(fyk.con) :UeT$=UeT.con$ '

iniciales=1 '

return '

'.....................................................................

[datos] 'lee datos de la pantalla izquierda y asigna variables

#1.L, "!contents? b" :#1.H, "!contents? h" :#1.p, "!contents? bw"

#1.t, "!contents? hf":#1.tipo,"!contents? tipo":#1.nombre,"!contents? nombre$"

#1.Nd,"!contents? Nd" :#1.Md, "!contents? Md" :#1.myd, "!contents? Myd"

#1.re,"!contents? rec":#1.ch, "!contents? ch" :#1.ca, "!contents? ca"

#1.cf,"!contents? cf" :#1.nC, "!contents? nC" :#1.dC, "!contents? dC"

#1.nT,"!contents? nT" :#1.dT, "!contents? dT"

#1.e, "!contents? fck":#1.pe, "!contents? fyk"

if right$(fc$,1)="d" then fcd=val(fc$):fck=0

if right$(fy$,1)="d" then fyd=val(fy$):fyk=0

return

'------------------------------------------------------------------

[escribir.dat1] '

gosub [datos] '

gosub [escribir.datos.dat1] '

wait '

[escribir.datos.dat1]

'nombre nº fck fyk UeT Fue UeF Mdx Mdy UeM rec UeL nC dC nT dT b

h bw hf

'FS_R_D01 1 0 0 c 0 kN 4.12 0 mT 4 cm 0 0 0 16 40

25 0 0 '

'POLI_D05 28 99d 4000d k 110.59 T 8.85 8.85 mT 5 cm 222332 0 8 28 8

8 28 8 28 -22

#dat1 te$(nombre$ ,8);" ";te$(str$(tipo),2);" ";te$(fc$,4);" ";te$(fy$,5);"

";te$(UeT1$,1);" ";_

te$(str$(Nd),6);" ";te$(UeF$,3);" ";te$(str$(Md) ,5);" ";te$(str$(Myd) ,5);"

";te$(UeM$,3);" ";_

te$(str$(rec),3);" ";te$(UeL$,2);" ";te$(str$(nC),6);" ";te$(str$(dC),2);"

";te$(str$(nT) ,2);" ";_

te$(str$(dT),2);" ";te$(str$(b),3);" ";te$(str$(h),4);" ";te$(str$(bw),4);"

";te$(str$(hf),4)

return

'---------------------------------------------------------------

sub abrirdat '

if properties(6)=1 then call closedat '

if properties(6)=0 then '

UpperLeftX=DisplayWidth/3: WindowWidth =1.7*DisplayWidth/3 '

UpperLeftY=1 : WindowHeight=DisplayHeight*0.95*0.5 '

open "dat1" for text as #dat1 '

'**************************** '

#dat1 "!font courier new 14" '

#dat1 "!trapclose [closeDat]"; '

properties(6) = 1 '

else '

#dat1 "!cls";: call closedat '

end if '

end sub '

[closeDat] '

call closedat '

wait '

sub closedat '

if properties(6)=1 then close #dat1 :properties(6)=0'

end sub '********** '

'---------------------------------------------------

[AYUDA]

call abrirAyuda

wait

sub abrirAyuda

if properties(5) = 0 then

UpperLeftX= DisplayWidth/3 :WindowWidth =DisplayWidth/3

UpperLeftY= 1 :WindowHeight =DisplayHeight*0.95

open "AYUDA" for text as #5

'**************************

#5 "!trapclose [cerrarAyuda]";

properties(5) = 1

open "ayuda-ha_2.txt" for input as #6

'--------------------------------

#5 "!font "; "arial 10";

while eof(#6)=0:line input #6, a$: #5 a$:wend

close #6

end if

end sub

[cerrarAyuda]

call cerrarAyudas: wait

sub cerrarAyudas

if properties(5)=1 then close #5:properties(5)=0

end sub '*******

'---------------------------------------------

sub configuracion

global Usuario$, ch,ca,cf,fck.con,fyk.con,UeT.con$,aaa$,Dmin,Dmax,dM

open "config-ha.txt" for input as #conf

input #conf, a$,Usuario$

input #conf, a$,ch,a$,ca,a$,cf

input #conf, a$,fck.con,UeT.con$

input #conf, a$,fyk.con,aaa$

input #conf, a$,coe.poi

input #conf, a$,mo.di.ter

input #conf, a$,Dmin,a$

input #conf, a$,Dmax,a$

input #conf, a$,dM,a$

close #conf

end sub

'.................

[con]

call configuracion

call abrirCon

wait

'...........

sub abrirCon


UpperLeftX= DisplayWidth/3 :WindowWidth =DisplayWidth/3

UpperLeftY= 1 :WindowHeight =DisplayHeight*0.3

open "CONFIGURACION" for text as #con

'************************************

#con "!trapclose [cerrarCon]";

properties(12) = 1

open "config-ha.txt" for input as #conf

'----------------------------------------

#con "!font "; "Courier New 10";

while eof(#conf)=0:line input #conf, a$:#con a$: wend

close #conf

end if

end sub

[cerrarCon]

call cerrarCon: wait

sub cerrarCon

if properties(12)=1 then close #con:properties(12)=0

end sub

wait

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

[fin]

call closeGraphWindow

call closeTextWindow

close #1

if properties(5) =1 then close #5

if properties(6) =1 then close #dat1

if properties(7) =1 then close #ab

if properties(8) =1 then close #c

if properties(9) =1 then close #3d

if properties(10)=1 then close #col

if properties(12)=1 then close #con

end

'00000000000000000000000000000000000000000000000000000000

[chubi] data 0.0581,0.2352,0.338,0.5,0.662,0.7648,0.9419

'oooooooooooooooooooooooooooooooooooooooooooooooooooooooo

[plot]

'oooooooooooooooooooooooooooooooooooooooooooooooooooooooo

plot=1 '

planta=1 '

if iniciales=0 then gosub [datos.iniciales] '

iniciales=0 '

call configuracion '

gosub [datos] '

if fileName$="" then hh=hh+1:notice noti$:wait

call openTextWindow 'abre la pantalla de resultados

perspectiva=0 '

if opc$="d" then '

ppd$=right$(pp$,9) : ppd$=left$(ppd$,8)'

ndg$="c:\dc\"+ppd$+".gra" '

open ndg$ for output as #3 '

#3 ndg$ : dc2=1 '

end if '

open pp$ for input as #d '

fff$=pp$ '

no=0 '

if len(str$(nC))>2 then [poligonal]

'-----------------------------------------------

gosub [unidades.salida] '

gosub [unidades.entrada] '

'*********************** '

if bw=0 then qq$="Rectangular" else qq$="T" '

if Md=0 then ww$="COMPROBACION" else ww$="DIMENSIONADO" '

#t ww$;" DE PIEZA DE H.A." '

#t "Seccion ";qq$;" - Metodo parabola-rectangulo." '

#t "__________________________________________________" '

#t "" '

restore [chubi]: for i=1 to 7:read a:ch(i)=a:next '

Mdd=Md '

if UeM$="mkN" then Md=Md/10 'paso de mkN a mT '

'resistencias de materiales '

fck=fck*CeTh : fyk=fyk*CeTa '

fcd=fcd*CeTh : fyd=fyd*CeTa '

if fcd=0 then fcd=fck/ch '

if Nd >0 and dC=0 then fcd=fcd*0.9 '

'unid. de calc. hor=T/m2 y ace=T/cm2 '

if fyd=0 then fyd=fyk/ca '

#t "MATERIALES" '

#t "Resistencia Caracteristica calculo" '

#t " ";UeT$ '

#t "Hormigon = ";c2$(fck/CeTh);" ";c2$(fcd/CeTh) '

#t "Acero = ";c2$(fyk/CeTh);" ";c2$(fyd/CeTa) '

#t "__________________________________________________" '

if len(COdA$)>2 then [poligonal] '

b=b*CeL : h=h*CeL '

rec=rec*CeL 'Recubrimiento mecanico a ejes (m) '

d=h-rec '

dC.min=10 'NP=nC 'nº de redondos compresion '

if dT=0 then dT=10 'diametro minimo armadura traccion mm'

'nnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn

if Nd>0 and Myd=0 then [dimen.compuesta]

if Myd>0 then [esviada]

'nnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn

aH=b*h ':secte=0

Dn=0

if bw>0 then

bw=bw*CeL: hf=hf*CeL 'escuadria seccion en T

secte=1 : aH=b*hf+bw*(h-hf)

end if

'................

aC=pi*nC*dC^2/400 'area de armadura a Compresion cm2

if fyd<3.41 or fyd>3.73 then [a]

ROmin=0.0033 : goto [b] 'cuantia geometrica minima

[a] if fyd<4.25 or fyd>4.64 then [c]

ROmin=0.0028 : goto [b]

[c] ROmin=0.016/(fyd+1.3)

[b] Amin =10000*aH*ROmin 'area min de armadura de traccion en cm2

'...................... ' NPA=nC

FCmax=0.85*fcd 'tension max del diagrama parabola-rectangulo

antonio=0 'canto util

[nuevo.calculo]

x1=0.628 : x=x1 'profundidad limite

'......................................................

if Mdd=0 then Md=Mdd: goto [comprobacion]

'******************************************************

' dimensionado flexion simple

nBl=0 : if h-hf>0.3 then nBl=int((h-hf)/(Dmax/100))+2

gosub [dimensionar]

'******************

if mu<=Md then [ddn] ' necesita mas armadura de compresion

e1=erm : x2=0.2 :ppp=erm ' error y nuevo tanteo

while abs(erm)>0.0001 ' busqueda de posicion de la linea neutra

x=x2 : gosub [dimensionar] ' error del ultimo tanteo

e2=erm: gosub [correccion]

wend

goto [nns]

[ddn]

Dn=(Md-mu)/(d-rec):nu=nu+Dn ' incremento de axil

da=Dn/s1 :aC=aC+da ' incremento de area

[nns]

if dC=0 then dC=dM

abarp=pi*dC^2/400 ' area de 1 barra a compresion cm2

nC=aC/abarp ' nº de barras a compresion

n.C=nC

nsT=nu 'axil de la armadura a traccion

s2=0.21*epsm*(1-x)/x : if abs(s2)>fyd then s2=fyd*sgn(s2) 'tension

aT =nsT/s2 : if aT<Amin then aT=Amin 'area total calculada cm2

abar=pi*dT^2/400 'area de 1 barra s/datos

iniciales

n.T =aT/abar: nT=n.T : if nT>int(n.T) then nT=int(n.T)+1 'nº de barras

s/calculo

AaC=ns+Dn :MaC=ms+erm 'axil del acero a compresion

AhC=nc :MhC=mc 'axil hormigon a "

AaT=nsT :MaT=Md 'Axil acero a traccion

gosub [flexion.simple]

'*********************

if dC=0 then dC=dC.min

if nC>int(nC) then nC=int(nC)+1

#t "Area <min> T = ";d2$(Amin);" cm2"

#t "Nº de barras ajustados T = ";d0$(nT);" d/ ";d0$(dT) ;" mm"

nT.min=int((b-2*rec)/(Dmax/100))+2 : if nT<nT.min then nT=nT.min

base=b:if bw>0 then base=bw

basE=base-2*rec

nT1=int((basE)/(dT/1000+Dmin/100)+1)

if nT1>= nT then nT1=nT : nT2=0

if nT1< nT then nT2=nT-nT1 : if nT2=1 then nT2=2

#t "nº de redondos en capa 1 = ";d0$(nT1);_

" dis.libre = ";t0$(1000*basE/(nT1-1)-dT);" mm"

aT1=nT1*pi*dT*dT/400 : #t "Area de acero en capa 1 = ";d2$(aT1)

if nT2=0 then [res.cal]

aT2 =aT-aT1 : #t "Area de acero en capa 2 = ";d2$(aT2)

abar.capa2=aT2/nT2 'area de 1 barra de capa 2

dT2=int(sqr(abar.capa2*400/pi))+1 'diametro de barras en capa 2

if dT2>16 and dT2<20 then dT2=20

if dT2>20 and dT2<25 then dT2=25

#t "Diametro de acero capa 2 = ";d0$(dT2)

#t "nº de redondos en capa 2 = ";d0$(nT2);_

" dis.libre = ";t0$(1000*basE/(nT2-1)-dT2);" mm"

if nT> nT1 and antonio<>1 then

antonio=1

d=d-(dT+Dmin*10)/1000/2

#t "nuevo canto util d = ";d2$(d);" m": goto [nuevo.calculo]

end if

#t "__________________________________________________"

goto [res.cal]

'vvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvv

'vvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvv

[comprobacion]

Md=0 : nBl=0

if nC=0 then nC=nC.min

if dC=0 then dC=dC.min

aT =pi*nT*dT*dT/400 'area de la armadura de traccion

nT1=nT : nT2=0

'.................

x2=0.1 : gosub [comprobar]

e1=nu : if nu<=0 then [kkk]

while abs(nu)>0.0001

x=x2 : gosub [comprobar]

e2=nu: gosub [correccion]

wend

[kkk]

AaC=aC*s1 :MaC=ms 'axil y momento del acero a compresion

AhC=nc :MhC=mc 'axil " hormigon a "

AaT=aT*s2 :MaT=mu 'Axil " acero a traccion

gosub [flexion.simple]

goto [res.cal]

'----------------------------------------------------------

[flexion.simple]

#t "DATOS INICIALES"

#t "Escuadria de la pieza (b x h) = ";d0$(b*100);"x";d0$(h*100);

if bw>0 then #t "x";d0$(bw*100);"x";d0$(hf^100) else #t ""

if Md>0 then

#t "Momento de calculo = ";t2$(Md*CsM);" ";mo$ ' mT

else

#t "Armadura inicial de compresion ";d2$(nC);" r dia= ";d0$(dC);" mm"

#t "Armadura inicial de traccion ";d2$(nT);" r dia= ";d0$(dT);" mm"

end if

#t "__________________________________________________"

#t "CALCULOS DEL HORMIGON Y ACERO A COMPRESION"

#t "Profundidad de la linea neutra xd = ";d2$(xd*CsL);" ";lo$ ' m

#t ""

#t " Axil Momen. Tension Deforma. Area nº"

#t " T mT N/mm2 o/oo<max cm2 cal ajus "

#t "Acero a COMPRESION ";t2$(AaC);" ";d2$(MaC);" ";t2$(s1*100);" ";_

d2$(aC);" ";d2$(n.C);" ";d0$(nC)

#t "Hormigon ";t2$(AhC);" ";d2$(MhC);" ";t2$(FCmax/100);" ";_

d0$(epsc1);" ";d0$(epsm)

#t "Acero de TRACCION ";t2$(AaT);" ";d2$(MaT);" ";t2$(s2*100) ;" ";_

d0$(0.21*epsm);" ";d2$(aT);" ";d2$(n.T);" ";d0$(nT)

#t

"______________________________________________________________________________"

nC.min=int((b-2*rec)/(Dmax/100))+2

if bw>0 and nC.min<4 then nC.min=4

if nC<nC.min then nC=nC.min

#t "nº de barras minima por ancho C = ";d0$(nC.min);" d/ ";d0$(dC.min);" mm"

#t "nº de barras ajustado en ancho C = ";d0$(nC) ;" d/ ";d0$(dC) ;" mm"

return

'-----------------------------------------------------

[correccion] ' correccion regula falsi

dx=(x1-x2)/(e1-e2)*e2 : if abs(dx)>0.2 then dx=0.2*sgn(dx)

if dx>x2 then dx=x2-0.01 ' evitar valores negativos

x1=x2 : e1=e2 : x2=x2-dx ' nuevos valores tanteo

return

'=============================================================

[dimensionar]

gosub [comun.resulta]

ns=aC*s1 : ms=aC*s1*(d-rec) 'axil y momento armadura C

nu=nc+ns : mu=mc+ms 'axil y momento ultimo

erm=Md-mu 'error en momentos

return

'...................................

[comprobar] 'COMPROBACION

gosub [comun.resulta]

s2=0.21*epsm*(1-x)/x : if abs(s2)>fyd then s2=fyd*sgn(s2)'Tension armadura T

ns=aC*s1-aT*s2 : ms=aC*s1*(d-rec) 'axil y momento de las armaduras

nu=nc+ns : mu=mc+ms 'axil y momento ultimo

return

',,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,

[comun.resulta]

if x<0.2593 then epsm=100*x/(1-x) else epsm=35

xd=x*d 'profundidad de la linea neutra

nc=0:mc=0 'esfuerzos hormigon

if bw=0 or xd<=hf then [uu1]

u1=0 :u2=hf:bu=b :gosub [integra] 'seccion T zona del ala

u1=hf:u2=xd:bu=bw :gosub [integra] ' " " zona del nervio

goto [ss1]

[uu1] u1=0:u2=xd:bu=b:gosub [integra] 'seccion rectangular

[ss1] s1=0.21*epsm*(x-rec/d)/x : if abs(s1)>fyd then s1=fyd*sgn(s1) 'tension C

return

'.........................................

[integra] '

du=u2-u1 '

for i=1 to 7 '

u=u1+du*ch(i) '

epsc=epsm*(x-u/d)/x 'deformacion del hormigon '

if i=1 then epsc1=epsc '

sigc=FCmax 'tension del hormigon '

if epsc<=20 then F=1-epsc/20: sigc=FCmax*(1-F*F) '

dn=sigc*bu*du/7 'axil fibra '

nc=nc+dn '

mc=mc+dn*(d-u) '

next '

return '

'mmmmmmmmmmmmmmmmmmmmmmmmmmmmmmmmm

'vvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvv

[dimen.compuesta]

COdA=nC

q$="Soportes rectangulares de hormigon armado a flexo-compresion recta"

linea$=

"_________________________________________________________________________"

#t q$

#t " Dimensiones recubr.(cm) Momento Carga Cod_armado"

#t " ";d0$(b*100);" ";d0$(h*100);" ";d0$(rec*100);" ";_

d2$(Md);" ";d2$(Nd);" ";d0$(COdA)

#t linea$

#t " CALCULO"

nBf=int(COdA/10) 'codigo de armado

nBl=COdA-10*nBf

#t "Numero de barras frontales ";d0$(nBf)

#t "Numero de barras laterales ";d0$(nBl)

if nBf=1 then nBf=2

n(1)=nBf:n(nBl)=nBf 'barras de la primera y ultima capa

y(1)=h/2-rec:y(nBl)=-1*y(1) 'profundidad de la primera y ultima capa

Dcapa=(h-2*rec)/(nBl-1)

#t "Distancia entre capas ";d2$(Dcapa);" m"

For i=2 to nBl-1

n(i)=2 'numero de barras de cada capa intermedia

y(i)=y(i-1)-Dcapa 'profundidad de cada capa

next

'd=h-rec

nBAR=2*(nBf+nBl)-4

#t "Canto util ";d2$(d);" m"

#t "Numero total de barras ";d0$(nBAR)

if dC>0 then [flexo.comp.comprobacion]

'*************************************

uMIN =40*b*h*fyd/nBAR 'capacidad mecanica minima de cada barra

EXmin=0.02*h/b

if EXmin<0.02 then EXmin=0.02

if EXmin<h/20 then EXmin=h/20

#t "Excentricidad minima ";d0$(EXmin*100);" cm"

if Md<0 then Md=-1*Md 'Solicitaciones

if Md<Nd*EXmin then Md=Nd*EXmin

#t "Momento flector (incluso excentricidad) ";d2$(Md);" mT"

x1=0.7*h:x2=0.71*h 'valores de tanteo de profundidad de la linea neutra

x3=x1:gosub [1710]:e1=erro 'error del primer tanteo

while abs(erro)>0.0001

x3=x2

gosub [1710]

e2=erro 'error del ultimo tanteo

dx=(x1-x2)/(e1-e2)*e2 'correccion regula falsi

if dx> 0.2*h then dx= 0.2*h 'valor maximo de la correccion

if dx<-0.2*h then dx=-0.2*h 'valor minimo de la correccion

if Nd>0 and dx*e2>0 then dx=-1*dx 'direccion equivocada

if dx>x2 then dx=x2-0.01 'evitar valores negativos

x1=x2:e1=e2:x2=x2-dx 'nuevos valores de tanteo

wend

aBAR=(Md-Mc)/Ms 'area de una barra

uBAR=aBAR*fyd 'capacidad mecanica de una barra

if uBAR<uMIN then uBAR=uMIN : aBAR=uMIN/fyd

diam=20*sqr(aBAR/pi) 'diametro de una barra

#t "Capacidad mecanica-1 barra y diametro-barras ";d2$(uBAR);" ";d2$(diam)

#t "Capacidad mecanica-cara ";d2$(uBAR*nBf)

xd=x3

goto [res.cal]

'----------------------------------------------------------------------------

'----------------------------------------------------------------------------

[comun.compuesta] 'Resultante Calculo de una fibra neutra

x=x3/d 'profundidad relativa de la fibra neutra

if x>0.1667 then [1770] 'dominio 2a

fi =4.25*x*(3-8*x)/(3*(1-x)^2) 'parametro axil relativo

lambda=(4-9*x)/(12-32*x) 'parametro profundidad relativa

epsc =100*x/(1-x):goto [1900] 'deformacion fibra superior

[1770] if x>0.2593 then [1810] 'dominio 2b

fi =0.85*(16*x-1)/15/x

lambda=(171*x^2-22*x+1)/(320*x^2-20*x)

epsc =100*x/(1-x):goto [1900]

[1810] if x3>h then [1850] 'dominios 3 y 4

fi =0.688095

lambda=0.415966

epsc =35 :goto [1900]

[1850]

x=x3/h 'dominio 5: nueva definicion de x

fi =0.85*(1-64/(21*(7*x-3)^2))

lambda=3*(2401*x^2-2058*x+185)/(14*(1029*x^2-882*x+125))

epsc =20*x/(x-3/7)

[1900] if x3>h then [1940] : 'axil y momento del hormigon

Nc=x3*b*fcd*fi : Mc=Nc*(h/2-x3*lambda) : goto [1960]

[1940] Nc=h*b*fcd*fi : Mc=Nc*h*(0.5-lambda)

[1960]

Ns=0:Ms=0 'axil y momento armaduras

epss=0.21*epsc 'valor auxiliar calculo de tension (sigs)

for i=1 to nBl 'en cada capa de armaduras

sigs=epss*(x3+y(i)-h/2)/x3

if sigs<-1*fyd then sigs=-1*fyd

if sigs> fyd then sigs= fyd

Ns=Ns+sigs*n(i)

Ms=Ms+sigs*n(i)*y(i)

next i

return

'..............

[1710]

gosub [comun.compuesta]

Nf=(Nd-Nc):Mf=(Md-Mc)

erro=(Nf-Ns*Mf/Ms)/Nd

return

'nnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn


[flexo.comp.comprobacion]

pepe=0

diam=dC

Nd.1=Nd 'guardamos el dato para la 2ª comprobacion: el mom max con este axil

'...........................................................................

aMIN=40*b*h/nBAR 'area minima por barra

aBAR=pi*diam*diam/400

if aBAR<aMIN then print "No cumple cuantia minima"

EXmin=0.02*h/b

if EXmin<0.02 then EXmin=0.02

if EXmin<h/20 then EXmin=h/20

#t "Excentricidad minima ";d0$(EXmin*100);" cm"

#t "Diametro de las barras ";dC;" mm"

#t ""

'.....................................

[nuevoC]

' Solicitaciones

if Md<0 then Md=-1*Md

EX=Md/Nd

if EX<EXmin then EX=EXmin

if EX>h then

EX=1/EX : KEX=1

else

KEX=0

end if

x1=0.6*h:x2=0.9*h 'valores de tanteo de profundidad de la l.neutra

x3=x1 :gosub [1710a] : e1=erro 'error del primer tanteo

while abs(erro)>0.0001

x3=x2 :gosub [1710a] : e2=erro 'error del ultimo tanteo

dx=(x1-x2)/(e1-e2)*e2 'correccion regula falsi

if dx> 0.2*h then dx= 0.2*h 'valor maximo de la correccion

if dx<-0.2*h then dx=-0.2*h 'valor minimo de la correccion

if Nd>0 and dx*e2>0 then dx=-1*dx 'direccion equivocada

if dx>x2 then dx=x2-0.01 'evitar valores negativos

x1=x2:e1=e2:x2=x2-dx 'nuevos valores de tanteo

wend

'if pepe=1 then [fin2]

c.s=nu/Nd 'coeficiente de seguridad

'if c.s<0.97 then Md=int(mu):#t "Momento flector excesivo. Md maximo = ";t2$(mu)

'if c.s<0.97 then Nd=Nd-0.5 :goto [nuevoC]

'if c.s>1.001 then Nd=Nd+0.5 :goto [nuevoC]

#t "Para un mom flector = ";t2$(Md);" mT ";"el Axil max = ";t2$(nu);" T "

#t "Coeficente de seguridad de axiles nu/Nd = ";d4$(nu/Nd)

#t "Coeficente de seguridad de momentos mu/Md = ";d4$(mu/Md)

#t "---------------------------------------------------"

[fin2]

if pepe=0 then Nd=Nd.1: pepe=1

c.s=nu/Nd

Mdmin=EXmin*Nd

if Md<Mdmin then

Md=Mdmin

#t "Momento flector escaso Md minimo = ";t2$(Md)

Nd=int(nu)

#t "Axil maximo = ";t2$(Nd)

'goto [nuevoC]

end if

'if c.s<1 then Md=Md-0.1: goto[nuevoC]

'if c.s>1.01 then Md=Md+0.1: goto[nuevoC]

[fin3]

#t "Para un axil = ";t2$(Nd);" T ";"el Mom flector max = ";t2$(mu);" mT "

#t "Coeficente de seguridad de momentos mu/Md = ";d4$(mu/Md)

#t "Coeficente de seguridad de axiles nu/Nd = ";d4$(nu/Nd)

[fin4]

xd=x1

goto [res.cal]

'------------------------------------------------

[1710a]

gosub [comun.compuesta]

nu=Nc+Ns*aBAR:mu=Mc+Ms*aBAR

if KEX=0 then eu=mu/nu else eu=nu/mu

erro=eu-EX

return



[esviada]

linea$="_____________________________________________________________________"

#t "Soportes rectangulares de hormigon armado a flexo-compresion esviada"

Mxd=Md

COdA=nC

U =0

Ut =0

Mxs=0

Mys=0

xi =0

errN=0

errM=0

#t "Calculo con diagrama de parabola-rectangulo"

#t " DATOS"

#t linea$

#t " Dimensiones recubr.(cm) Momento Carga Cod_armado Diam"

#t " ";d0$(b*100);" ";d0$(h*100);" ";d2$(rec*100);" ";d2$(Mxd);"

";_

d2$(Myd);" ";d2$(Nd);" ";d0$(COdA);" ";d0$(diam)

#t linea$

#t " CALCULO"

hx=b :hy=h

cx=rec/hx :#t "recubrimientos reducido en x ";d2$(cx)

cy=rec/hy :#t "recubrimientos reducido en y ";d2$(cy)

facN =0.85*fcd*hx*hy :#t "Axil maximo del hormigon ";t0$(facN);" T"

facMy=facN*hx

facMx=facN*hy

'codigo de armado

nBf=int(COdA/10) :nx=nBf :#t "Numero de barras frontales ";d0$(nBf)

nBl=COdA-10*nBf :ny=nBl :#t "Numero de barras laterales ";d0$(nBl)

nBAR=2*(nBf+nBl)-4 :#t "Numero total de barras ";d0$(nBAR)

n(1)=nBf 'barras de esquina

n(2)=nBf+nBl-1

n(3)=n(2)+nBf-1

n(4)=nBAR

EXmin=hx/20 : if EXmin<0.02 then EXmin=0.02

EYmin=hy/20 : if EYmin<0.02 then EYmin=0.02

#t "Excentricidad minima EXmin = ";d0$(EXmin*100);" cm"

#t "Excentricidad minima EYmin = ";d0$(EYmin*100);" cm"

sx=(1-2*cx)/(nBf-1) : x=0.5-cx : dx=-1*sx

sy=(1-2*cy)/(nBl-1) : y=0.5-cy : dy=0

rag=180/pi

if Mxd<0 then Mxd=-1*Mxd

if Myd<0 then Myd=-1*Myd

if Nd <1 then Nd=1 'axil minimo

EX=Myd/Nd : EY=Mxd/Nd

if dC>0 then [esviada.comprobacion]

'------------------------------------

uMIN=40*hx*hy*fyd/nBAR 'capacidad mecanica min de 1 barra

'Solicitaciones

fi=90

if EX>=EXmin or EY>=EYmin then [1610]

#t "hx hy ";hx;" ";hy

if hx>=hy then [1590]

EX=EXmin : Myd=EX*Nd

' EY=0 : Mxd=0 : goto [1620]

EY=EYmin : Mxd=EY*Nd : goto [1620]

[1590] EY=EYmin : Mxd=EY*Nd

' EX=0 : Myd=0


[1610] if EX<>0 then fi=rag*atn((EY/EX)*(hx/hy))

[1620] bet=fi

xi=0.7

#t "Excentricidad calculada EX = ";d2$(EX*100);" cm"

#t "Excentricidad calculada EY = ";d2$(EY*100);" cm"

#t "Momento de calculo Mxd = ";d2$(Mxd);" mT"

#t "Momento de calculo Myd = ";d2$(Myd);" mT"

gosub [1880]

'***********

while abs(errN)>0.0001 or abs(errM)>0.001 'nuevo i

xi1=xi : e5=errN : xi=xi1+0.01

while abs(errN)>0.0001

gosub [1880]

'***********

dxi=((xi1-xi)/(e5-errN))*errN

if abs(dxi)>0.2 then dxi=0.2*sgn(dxi)

if dxi*errN>0 then dxi=-1*dxi

xi1=xi : e5=errN : xi=xi-dxi

if xi>2 then xi=2

if xi<0 then xi=0.01

wend

bet1=bet : e6=errM : bet=bet1+1

while abs(errM)>0.001

gosub [1880]

'***********

dbet=(bet1-bet)/(e6-errM)*errM

if abs(dbet)>36 then dbet=36*sgn(dbet)

bet1=bet : e6=errM : bet=bet-dbet

if bet>90 then bet=90

if bet<0 then bet=0

wend

wend

#t "Angulo de la fibra neutra bet = ";d2$(bet1);" º"

#t "area de cada barra = ";d2$(aBAR);" cm2"

uBAR=aBAR*fyd : if uBAR<uMIN then uBAR=uMIN 'capacidad mecanica de una

barra

FI=20*sqr(uBAR/pi/fyd)

#t "diametros de las barras = ";d2$(FI);" mm"

#t "Capacidad mecanica 1 barra = ";d2$(uBAR);" T"

#t "Capacidad mecanica total = ";d2$(nBAR*uBAR);" T"

#t "Canto util oblicuo = ";d2$(D)

if bet1>90 then bet1=bet1-90

be=bet1*pi/180 'angulo de la linea neutra en radianes

D1=(h+(b)*tan(be))*cos(be)

Uo=x1*D1

#t "profundidad oblicua = ";d2$(Uo);" m"

h1=Uo/cos(be)

h2=b*tan(be)

h3=h-h1+h2

if h3<=h then xA=0:yA=h3 else xA=b-Uo/sin(be) :yA=h

if h1<=h then xB=b:yB=h-h1 else xB=(h2-(h1-h))/tan(be):yB=0

#t "Coordenadas xA yA ";d2$(xA);" ";d2$(yA)

#t "Coordenadas xB yB ";d2$(xB);" ";d2$(yB)

diam=FI

goto [res.cal]

'--------------------------------------------------------------

'oooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooo

[comun]

if bet<=45 then T=tan(bet/rag) else T=tan((90-bet)/rag)

T1=1/(1+T) : T2=1-T1

C=1/sqr(1+T*T) : S=T*C 'coseno y seno

D=((1-cx)*C+(1-cy)*S)/(C+S) 'canto util oblicuo

if xi>0 then [1950a]

epsc=100*xi :epss=-100 :goto [2030a]

[1950a] if xi>0.2593*D then [1980a]

epsc=100*xi/(D-xi) :epss=-100 :goto [2030a]

[1980a] if xi>1 then [2010a]

epsc=35 :epss=35*(xi-D)/xi:goto [2030a]

[2010a] epsc=50-15*xi:eps=35*(1-D):epss=eps+(xi-1)*(20-eps)

[2030a] deps=(epsc-epss)/D/(C+S)

Nc=0 : Mxc=0 : Myc=0 'resultante hormigon

if xi<T2 then x1=xi else x1=T2

gosub [triangulo]

'****************

if xi<=T2 then [2130a]

if xi< T1 then x1=xi else x1=T1

gosub [paralelogramo]

'********************

if xi<=T1 then [2130a]

if xi< 1 then x1=xi else x1=1

gosub [trapecio]

'***************

[2130a]

if bet<=45 then [2160a]

m3=Myc : Myc=Mxc : Mxc=m3

T=S : S=C : C=T

[2160a] Nc=Nc*facN : Mxc=Mxc*facMx : Myc=Myc*facMy

Ns=0 : Mxs=0 : Mys=0

U=cx*C+cy*S : du=C*sx

for i=1 to nBAR

eps=epsc-U*deps

sig=0.21*eps

if sig<-1*fyd then sig=-1*fyd

if sig> fyd then sig= fyd

Ns=Ns+sig

Mxs=Mxs+sig*y

Mys=Mys+sig*x

if i=n(1) then dx=0 : dy=-1*sy : du= S*sy 'esquinas

if i=n(2) then dx=sx : dy=0 : du=-1*C*sx

if i=n(3) then dx=0 : dy= sy : du=-1*S*sy

x=x+dx : y=y+dy : U=U+du

next

dx=-1*sx :dy=0

return

'****************************************************************

[1880]

'*****

gosub [comun]

'************

Mxs=Mxs*hy : Mys=Mys*hx

if abs(Ns)<=0.1 then [2370]

aBAR=(Nd-Nc)/Ns : goto [2400]

[2370] if abs(Mxs)<=0.1 then [2390]

aBAR=(Mxd-Mxc)/Mxs : goto [2400]

[2390] aBAR=(Myd-Myc)/Mys

[2400] Nr=Nd-Nc : Mxr=Mxd-Mxc : Myr=Myd-Myc

if abs(Myd)>abs(Mxd) then [2460]

errN=(Nr-Mxr*Ns/Mxs)/Nd

errM=(Mxr*Mys/Mxs-Myr)/Mxd

goto [2480]

[2460] errN=(Nr-Myr*Ns/Mys)/Nd

errM=(Mxr-Myr*Mxs/Mys)/Myd

[2480] return

'.......................

[triangulo]

'**********

if T2=0 then return

ht=S*x1/T2 'altura total del triangulo

for i=1 to 7

U=ch(i)*ht 'profundidad de la franja

eps=epsc-U*deps 'deformacion del hormigon

sig=1 'tension relativa

if eps<20 then aux=1-eps/20 : sig=1-aux*aux

sig=sig*ch(i) 'axil franja

Nc=Nc+sig : Mxc=Mxc+sig*(1-U/S) : Myc=Myc+sig*(1-U/C)

next i

fac=ht*ht/S/C/14

Nc=2*Nc*fac : Mxc=Mxc*fac : Myc=Myc*fac

return

'.....................................

[paralelogramo] '

'************** '

if T2=0 then ht=x1 else ht=S*(x1/T2-1) '

Np=0 : My=0 : x0=(1-T)/2 '

for i=1 to 7 '

U=S+ch(i)*ht '

eps=epsc-U*deps :sig=1 '

if eps<20 then aux=1-eps/20 :sig=1-aux*aux '

Np=Np+sig : My=My+sig*(x0-(U-S)/C) '

next i '

fac=ht/C/7 '

Nc=Nc+Np*fac : Myc=Myc +My*fac '

return '

'..........................

[trapecio]

'*********

if T2=0 then return

ht=(C+S)*x1-C

Np=0 : Mx=0 : My=0

for i=1 to 7

U=C+ch(i)*ht

eps=epsc-U*deps : sig=1

if eps<20 then aux=1-eps/20 : sig=1-aux*aux

sig=sig*(S-ch(i)*ht)

Np=Np+sig : Mx=Mx+sig*(C-U)/S : My=My+sig*(S-U)/C

next i

fac=ht/S/C/14

Nc =Nc+Np*2*fac : Mxc=Mxc+Mx*fac : Myc=Myc+My*fac

return

'.........................

'SSSSSSSSSSSSSSSSSSSSSSSSS

[esviada.comprobacion]

diam=dC

#t "Comprobacion de seccion a flexion compuesta esviada"

aMIN=40*hx*hy/nBAR

aBAR=pi*diam*diam/400

if aBAR<aMIN then #t "no cumple cuantia minima"

if EX>= EXmin or EY>=EYmin then [1620a]

if hx>= hy then [1590a]


EY=0 : Mxd=0 : goto [1620a]

[1590a] EY=EYmin : Mxd=EY*Nd

EX=0 : Myd=0

[1620a] fi=90

if EX<>0 then fi=rag*atn((EY/EX)*(hx/hy))

#t "Excentricidad calculada EX = ";d0$(EX*100);" cm"

#t "Excentricidad calculada EY = ";d0$(EY*100);" cm"

RO=sqr(EX*EX+EY*EY) 'distancia origen. excentricidad total

if RO>sqr(hx*hx+hy*hy)/2 then RO=1/RO :KEX=1 else KEX=0

bet=fi : xi=0.5

gosub [1880a]

'************

while abs(errRO)>0.001*RO or abs(errAN)>0.1

xi1=xi : e5=errRO : xi=xi1+0.1 'nuevo valor de xi

while abs(errRO)>0.001*RO

gosub [1880a]

'************

dxi=((xi1-xi)/(e5-errRO))*errRO


if dxi*errRO>0 then dxi=-1*dxi

xi1=xi : e5=errRO : xi=xi-dxi

if xi>2 then xi=2


wend

bet1=bet : e6=errAN : bet=bet1+9

while abs(errAN)>0.1

gosub [1880a]

'************

dbet=(bet1-bet)/(e6-errAN)*errAN

if abs(dbet)>9 then dbet=9*sgn(dbet)

bet1=bet : e6=errAN : bet=bet-dbet

if bet>90 then bet=90

if bet<0 then bet=0

wend

wend

#t "Axil ultimo Nu = ";d2$(Nu);" T"

#t "Momento x ultimo Mxu = ";d2$(Mxu);" mT"

#t "Momento y ultimo Myu = ";d2$(Myu);" mT"

if bet1>90 then bet1=bet1-90

be=bet1*pi/180 'angulo de la linea neutra en radianes

D1=(h+(b)*tan(be))*cos(be)

Uo=x1*D1

#t "profundidad oblicua = ";d2$(Uo);" m"

h1=Uo/cos(be)

h2=b*tan(be)

h3=h-h1+h2

if h3<=h then xA=0:yA=h3 else xA=b-Uo/sin(be) :yA=h

if h1<=h then xB=b:yB=h-h1 else xB=(h2-(h1-h))/tan(be):yB=0

#t "Coordenadas xA yA ";d2$(xA);" ";d2$(yA)

#t "Coordenadas xB yB ";d2$(xB);" ";d2$(yB)

diam=dC

c.s=Nu/Nd 'coeficiente de seguridad

#t "Coeficiente de seguridad ";d2$(c.s)

if c.s<0.97 then Md=int(mu):#t "Falta armadura "

' Momento flector excesivo. Mxu maximo = ";t2$(Mxu)

goto [res.cal]

'-------------------------------------------------------------------

'*******************************************************************

[1880a]

'******

gosub [comun]

Ns=Ns*aBAR : Mxs=Mxs*aBAR*hy : Mys=Mys*aBAR*hx 'paso del reducido al real

Nu=Nc+Ns : Mxu=Mxc+Mxs : Myu=Myc+Mys 'esfuerzos ultimos

Exu=Myu/Nu : Eyu=Mxu/Nu 'excentricidades resultantes

ROU=sqr(Exu*Exu+Eyu*Eyu)

if KEX=1 then ROU=1/ROU

errRO=ROU-RO 'error radial

if abs(Exu)>=0.0001 then [2470a]

errAN=90-fi 'error angular

goto [2480a]

[2470a] errAN=rag*atn(Eyu/Exu*hx/hy)-fi

[2480a] return

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

'------------------------------------------------------------------------

'---------------------POLIGONAL-----POLIGONAL----------------------------

[poligonal]

q$="Soportes poligonales de hormigon armado a flexo-compresion esviada"

linea$="_______________________________________________________________________"

nBAR=0

diam=0

bw=0

COdA$=str$(nC)

ndv=len(COdA$)

Mxd=Md

for n=1 to ndv: x(n)=x(n)/100:y(n)=y(n)/100:next

x(ndv+1)=x(1):y(ndv+1)=y(1) 'cierre poligonal

'.......................

'resistencias de calculo

fcd=fcd*8.5 : fyd=fyd/1000

#t q$

#t " DATOS"

#t " Hormigon Acero"

#t "Resistencia de calculo (kg/cm2) ";q2$(fcd/8.5);" ";q2$(fyd*1000)

#t linea$

#t " rec.(cm) x.Momentos.y Carga Cod_armado diam"

#t " ";d2$(rec);" ";d2$(Mxd);" ";d2$(Myd);" ";t2$(Nd);" ";COdA$;"

";d0$(diam)

#t linea$

#t " CALCULO"

betMIN=-90 : betMAX=270

xMIN=1000 : yMIN=1000 :xMAX=-1000 :yMAX=-1000 :aH=0

for n=1 to ndv

aH=aH+(y(n+1)+y(n))*(x(n+1)-x(n))/2 'area de hormigon

if x(n)<xMIN then xMIN=x(n)

if x(n)>xMAX then xMAX=x(n)

if y(n)<yMIN then yMIN=y(n)

if y(n)>yMAX then yMAX=y(n)

next

hx=xMAX-xMIN: exMIN=hx/20 :if exMIN<0.02 then exMIN=0.02 'excentricidad minima

hy=yMAX-yMIN: eyMIN=hy/20 :if eyMIN<0.02 then eyMIN=0.02

rec=rec/100

#t "Area de hormigon = ";d2$(aH);" m2"

#t "Recubrimiento mecanico = ";d2$(rec)

#t "Codigo de armado por caras = ";

for n=1 to ndv : N(n)=val(mid$(COdA$,n,1)):#t N(n);" ";:next 'barras por cara

#t ""

#t " Coordenadas"

#t "Vertices barras de esquina"

for n=1 to ndv

nBAR=nBAR+N(n)

sA2(n)=0:eR=0:gosub [paralela]

xs(n)=xx : ys(n)=yy 'coordenada barra de esquina en vertice n

next

xs(ndv+1)=xs(1): ys(ndv+1)=ys(1) 'cierre poligonal

nBAR=nBAR-ndv 'numero de barras

a=-1*fcd/400: b=fcd/10

rag=180/pi

DbetMAX=(betMAX-betMIN)/10

uMIN =40*fyd*aH/nBAR 'capacidad mecanica minima de la barra

#t "Diferencia angular maxima DbetMAX = ";DbetMAX

#t "Numero de barras = ";d0$(nBAR)

#t "Capacidad mecanica minima de la barra = ";d2$(uMIN)

if Nd<1 then Nd=1

ex=Myd/Nd: ey=Mxd/Nd

fi=90 : if ey<0 then fi=-1*fi

if abs(ex)>= exMIN or abs(ey)>=eyMIN then [1820]

if hx>=hy then [1800]

ex=exMIN*sgn(ex): if ex=0 then ex=exMIN

Myd=ex*Nd : Mxd=0: ey=0: goto [1820]

[1800] ey=eyMIN*sgn(ey): if ey=0 then ey=eyMIN

Mxd=ey*Nd : Myd=0: ex=0

[1820] if ex=0 then [1850p]

fi=rag*atn((ey/ex)*(hx/hy))

if ex<0 then fi=fi+180

'-------------------------------------------------------------

[1850p] beta=fi : xi=0.7: gosub [2100]

'***********

#t d4$(xi);" ";d4$(beta);" ";d4$(en);" ";d4$(em)

'#t "Excentricidad minima exMIN y calculada ex = ";d0$(exMIN*100);"

";d2$(ex*100);" cm"

'#t "Excentricidad minima eyMIN y calculada ey = ";d0$(eyMIN*100);"

";d2$(ey*100);" cm"

while abs(en)>0.0001 or abs(em)>0.0001

xi1=xi : en1=en : xi=xi1+0.01

while abs(en)>0.0001

gosub [2100]

'***********

'#t d4$(xi);" ";d4$(beta);" ";d4$(en);" ";d4$(em)

dxi=((xi1-xi)/(en1-en))*en


if dxi*en>0 then dxi=-1*dxi

xi1=xi : en1=en : xi=xi-dxi

if xi>2 then xi=2


wend

'#t ""

beta1=beta : em1=em : beta=beta1+1

while abs(em)>0.0001

gosub [2100]

'***********

dbeta=((beta1-beta)/(em1-em))*em

if abs(dbeta)>DbetMAX then dbeta=DbetMAX*sgn(dbeta)

beta1=beta : em1=em: beta=beta-dbeta

#t d4$(xi);" ";d4$(beta);" ";d4$(en);" ";d4$(em)

if beta>betMAX then beta=betMAX

if beta<betMIN then beta=betMIN

wend

#t ""

wend

#t "Tensiones de trabajo fcd fyd = ";fcd;" ";fyd

#t "Area de una barra aBAR = ";d2$(aBAR)

U=aBAR*fyd

#t "Capacidad mecanica necesaria U = ";d2$(U)

if U<uMIN then U=uMIN

diam=20*sqr(U/fyd/pi)

#t "U diam (mm) = ";d2$(U);" ";d2$(20*sqr(U/fyd/pi))

b=xMAX-xMIN

h=yMAX-yMIN

R=0.015

e=0.008 'diametro del estribo

r=diam/2000

for n=1 to ndv

dis=sqr((x(n)-xs(n))^2+(y(n)-ys(n))^2) ' distancia vertice poli.-centro barr

sA2(n)=rec/dis

next n

'.................................................................

for n=1 to ndv :eR=R :gosub [paralela]

xs.e(n)=xx: ys.e(n) =yy : next 'vertices poligono int. estribos

xs.e(ndv+1) =xs.e(1) :ys.e(ndv+1)=ys.e(1) 'cierre poligonal

for n=1 to ndv :eR=R+e :gosub [paralela]

xs.a(n)=xx: ys.a(n) =yy : next 'vertices poli exterior estribos

xs.a(ndv+1) =xs.a(1) :ys.a(ndv+1)=ys.a(1) 'cierre poligonal

for n=1 to ndv :eR=0 :gosub [paralela]

xs.e1(n)=xx: ys.e1(n)=yy: next 'centros de mandriles de estribos

xs.e1(ndv+1)=xs.e1(1):ys.e1(ndv+1)=ys.e1(1) 'cierre poligonal

'.................................................................

for n=1 to ndv

h1=sqr((xs.e1(n)-xs.e(n))^2+(ys.e1(n)-ys.e(n))^2) 'dist cent.curva-vertice

estr.int

s1(n)=sqr(h1^2-R^2)

' d1(n)=2*R*s1(n)/h1

' alfa(n)=2*asn(d1(n)*0.5/R)*rag 'angulo de curva en el

mandril

alfa(n)=2*acs(R/h1)*rag

pp=n+1:if pp>ndv then pp=1

lado.e(n)=sqr((xs.e(pp)-xs.e(n))^2+(ys.e(pp)-ys.e(n))^2) 'lados poli.

int.estribos

next n

for n=1 to ndv

np=n+1:if np>ndv then np=1 'numero de vertice posterior a n

na=n-1:if na<1 then na=ndv 'numero de vertice anterior a n

x.man.a(n)=(xs.e(n )-xs.e(na))*s1(n)/lado.e(na)

y.man.a(n)=(ys.e(n) -ys.e(na))*s1(n)/lado.e(na)

x.man.p(n)=(xs.e(np)-xs.e(n)) *s1(n)/lado.e(n)

y.man.p(n)=(ys.e(np)-ys.e(n)) *s1(n)/lado.e(n)

gamma(n)=r.g*atn((y(n)-ys.e1(n))/(x(n)-xs.e1(n)))

next n

goto [res.cal]

'...................................................................

'-------------------------------------------------------------------

[paralela]

recu=rec+(R-r)*sA2(n)-eR

if n=1 then no=ndv : ne=1 else no=n-1:ne=n

gosub [3190]

'***********

dya=dy :dxa=dx: dza=dz

no=n :ne=n+1

gosub [3190]

'***********

dd=dy*dxa-dya*dx

xx=(dz*dxa-dza*dx)/dd 'coordenada vertice n poligono (sin curva)

yy=(dy*dza-dya*dz)/dd

return

'.........................................

[3190] 'coordenadas de puntos en la bisectriz de esquina

dy=y(ne)-y(no) : dx=x(no)-x(ne)

dz=dy*x(no)+dx*y(no) + recu*sqr(dx*dx+dy*dy)

return

'------------------------------------------------------------------

[2100]

xMIN=1000 :xsMIN=1000 : xMAX=-1000

S=sin(beta/rag) : C=cos(beta/rag)

if abs(C)<0.0001 then C=0 : S=sgn(S)

for n=1 to ndv+1 'coordenadas en ejes girados

xp(n)= x(n)*C+y(n)*S

yp(n)=-1*x(n)*S+y(n)*C

if xp(n)<xMIN then xMIN=xp(n) 'xMIN =vertice menos comprimido

if xp(n)>xMAX then xMAX=xp(n) 'xMAX = mas

next n

for n=1 to ndv 'abcisa girada de la barra

xsp(n)=xs(n)*C+ys(n)*S

if xsp(n)<xsMIN then xsMIN=xsp(n) 'xsMIN=barra menos comprimida

next n

xsp(ndv+1)=xsp(1)

d=(xMAX-xsMIN)/(xMAX-xMIN) 'canto util relativo oblicuo

if xi>0 then [2290]

epsc= 100*xi 'dominio 1

epss=-100 : goto [2380]

[2290] if xi>0.2593*d then [2320]

epsc= 100*xi/(d-xi) 'dominio 2

epss=-100 : goto [2380]

[2320] if xi>1 then [2350]

epsc=35 'dominios 3 y 4

epss=35*(xi-d)/xi : goto [2380]

[2350] epsc=50-15*xi 'dominio 5

eps=35*(1-d)

epss=eps+(xi-1)*(20-eps)

[2380]

Nc=0 : Mxc=0 : Myc=0 'resultante del hormigon

Ns=0 : Mxs=0 : Mys=0 ' de las armaduras

ae=(epsc-epss)/(xMAX-xsMIN)

be=epsc-ae*xMAX

x0=-1*be/ae : x20=(20-be)/ae 'abcisas para eps=0 y 20

for n=1 to ndv

x1=xp(n) : x2=xp(n+1) : signo=1 : yo=yp(n)

if x1=x2 then [2610]

if x1<x2 then [2490]

x1=xp(n+1) : x2=xp(n) : signo=-1: yo=yp(n+1)

[2490] if x2<=x0 then [2610]

ay=signo*(yp(n+1)-yp(n))/(x2-x1)

by=yo-ay*x1

if x1<=x0 then x1=x0

if x2>x20 then [2560]

xp1=x1 : xp2=x2 : n5=1 : gosub [trapeciop]

goto [2610]

[2560] if x1>=x20 then [2600]

xp1=x1 : xp2=x20: n5=1 : gosub [trapeciop]

xp1=x20: xp2=x2 : n5=0 : gosub [trapeciop]

goto [2610]

[2600] xp1=x1 : xp2=x2 : n5=0 : gosub [trapeciop]

[2610] next n

exc=Myc/Nc : eyc=Mxc/Nc 'excentricidades giradas

Mxc=Nc*(exc*S+eyc*C) 'esfuerzos a ejes generales

Myc=Nc*(exc*C-eyc*S)

for n=1 to ndv

x=xs(n): y=ys(n) : xp=xsp(n) : N=N(n)-1

dx=0 : dy=0 : dxp=0

if N=1 then [2710]

dx=(xs(n+1)-x)/N

dy=(ys(n+1)-y)/N : dxp=(xsp(n+1)-xp)/N

[2710] for j=1 to N

eps=ae*xp+be : sig=0.21*eps

if sig<-1*fyd then sig=-1*fyd

if sig>fyd then sig=fyd

Ns=Ns+sig : Mxs=Mxs+sig*y : Mys=Mys+sig*x

x=x+dx : y=y+dy : xp=xp+dxp

next j

next n

if abs(Ns)<=0.1 then [2810]

aBAR=(Nd-Nc)/Ns : goto [2840]

[2810] if abs(Mxs)<=0.1 then [2830]

aBAR=(Mxd-Mxc)/Mxs : goto [2840]

[2830] aBAR=(Myd-Myc)/Mys

[2840] Nf=Nd-Nc : Mxf=Mxd-Mxc 'diferencia para aceros

Myf=Myd-Myc

if abs(Myd)>=abs(Mxd) then [2900]

en=(Nf -Mxf*Ns /Mxs)/Nd 'error de axil

em=(Mxf*Mys/Mxs-Myf)/Mxd 'error de momentos

goto [2920]

[2900] en=(Nf - Myf*Ns /Mys)/Nd

em=(Mxf- Myf*Mxs/Mys)/Myd

[2920] if abs(abs(em)-pi)<0.001 then em=0

return

'-------------------------------------------------------------------------------

[trapeciop]

'*********

z1=xp1 : z2=xp2

for j=1 to 5

del(j)=(z2-z1)/j

z1=z1*xp1 : z2=z2*xp2

next j

if n5<>0 then [3030]

csig=fcd

asig=0

bsig=0

goto [3060]

[3030] asig= a*ae*ae

bsig=2*a*ae*be+b*ae

csig= a*be*be+b*be

[3060] f4=asig*ay

f3=bsig*ay+asig*by

f2=csig*ay+bsig*by

f1= csig*by

g5=f4*ay

g4=f3*ay+asig*ay*by

g3=f2*ay+bsig*ay*by+asig*by*by

g2=f1*ay+csig*ay*by+bsig*by*by

g1= csig*by*by

Nc =Nc +signo*(f4*del(4)+f3*del(3)+f2*del(2)+f1*del(1))

Mxc=Mxc+signo*(g5*del(5)+g4*del(4)+g3*del(3)+g2*del(2)+g1*del(1))/2

Myc=Myc+signo*(f4*del(5)+f3*del(4)+f2*del(3)+f1*del(2))

return

'oooooooooooooooooooooooooooooooooooooooooooooooooooo


[unidades.salida]

#1.UsL , "!contents? CsL$" : if CsL$="" then CsL$="m" : #1.UsL CsL$

#1.UsF , "!contents? CsF$" : if CsF$="" then CsF$="T" : #1.UsF CsF$

#1.UsM , "!contents? CsM$" : if CsM$="" then CsM$="mT": #1.UsM CsM$

If upper$(CsL$)="M" then CsL=1 :lo$="m." '

If upper$(CsL$)="CM" then CsL=100 :lo$="cm" '

if upper$(CsL$)="PU" then CsL=39.37 :lo$="pu" '

If upper$(CsF$)="T" then CsF=1 :fu$="T" '

If upper$(CsF$)="KN" then CsF=10 :fu$="kN" '

if upper$(CsF$)="KL" then CsF=2.2046:fu$="kL" '

if upper$(CsM$)="MT" then CsM=1 :mo$="mT" '

if upper$(CsM$)="MKN" then CsM=10 :mo$="mkN" '

return '

'----------------------------------------------------

[unidades.entrada]

#1.UeL , "!contents? CeL$" : if CeL$="" then CeL$="cm": #1.UeL CeL$

#1.UeF , "!contents? CeF$" : if CeF$="" then CeF$="T" : #1.UeF CeF$

if upper$(UeL$)="M" then CeL=1 '

if upper$(UeL$)="CM" then CeL=0.01 '

if upper$(UeL$)="PU" then CeL=1/39.37 '

if upper$(UeF$)="T" then CeF=1 '

if upper$(UeF$)="KN" then CeF=0.1 '

if upper$(UeF$)="KL" then CeF=1/2.2046 '

if upper$(UeT$)="KG/CM2" then CeTh=10 :CeTa=0.001 '

if upper$(UeT$)="N/MM2" then CeTh=100:CeTa=0.01 '

if upper$(UeT$)="MPA" then CeTh=100:CeTa=0.01 '

'

return '

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

[res.cal] 'RESULTADOS GRAFICO DEL CALCULO

close #d

'+++++++++++++++++++++++++++++++++++++++++++++++++++

call openGraphWindow '

#g "down ; size 1 ; color darkpink" '

w.w=WindowWidth : w.h=WindowHeight-150 '

e.h=0.7*w.w/b : e.v=0.7*w.h/h '

if e.h<e.v then esca=e.h else esca=e.v '

esca.per=esca : dim pp(Nnu) '

gosub [planta.alzado] '

wait


[des] '

if perspectiva=0 then dim segId(3*Nba) '

if planta=1 then gosub [planta.alzado] '


'

if dime=3 then '

d =1200/2 : d=d*ymax/xmax '

if d>600 then d=600 '

if d<500 then d=500 '

'

#1.r1,"!contents? r1": #1.r2,"!contents? r2": #1.r3,"!contents? r3"

#1.mx,"!contents? mx": #1.my,"!contents? my": #1.mz,"!contents? mz"

#1.kk,"!contents? kk" '

'

if r1=0 then r1=int(5.283*360/2/pi) : #1.r1 r1 '



if mx=0 then mx=0.5 : #1.mx mx '

if my=0 then my=0.5 : #1.my my '

if mz=0 then mz=-350 : #1.mz mz '

#1.kk kk '

r1=r1*g.r : r2=r2*g.r : r3=r3*g.r '

if perspectiva=1 then gosub [borrar.perspectiva] '

'

sr1=sin(r1): cr1=cos(r1) '



'

for n=1 to Nba '

x=x(n.i(n)):y=1*z(n.i(n)):z=y(n.i(n)) : gosub [310]:sxi=sx:syi=sy '

x=x(n.j(n)):y=1*z(n.j(n)):z=y(n.j(n)) : gosub [310]:sxj=sx:syj=sy '

#g "size 1 ; color red" '

#g "line ";w.w/2+esca.per*(sxi+mx);" ";h.p-esca.per*syi+300;" ";_ '

w.w/2+esca.per*(sxj+mx);" ";h.p-esca.per*syj+300;" "; '

' #t #g, "segment" '

input #g, segId(n) '

next n '

perspectiva=1 '

r1=r1*r.g : r2=r2*r.g : r3=r3*r.g '

'................................ '

#g "flush" '

#g "when rightButtonUp [cls]" '

#g "setfocus; down" '

#g "color black" '

#g "when leftButtonUp [setForLine]" '

'

[inputLoop] '

n=0 : m=0 '

segId=0 '

qqq=2 '

lineThickness$ = "1" '

lineColor$ = "black" '

end if '

wait '

'zzzzzzzzzzzzzzzzzzzzzzzzzzzzz

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

[planta.alzado] '

if fileName$="" or plot=0 then notice noti$:wait '

#1.esca, "!contents? escala" '

#1.tex5, "!contents? ttto" '

w.w=WindowWidth '

esca=esca+esca*escala/100 '

e2=esca/2/1000 '

if Nd>0 or Myd>0 then dM=diam: dT=diam: nT=nBf: dC=diam: nC=nBf: nT1=nT: nT2=0

rT=dT*e2 : rT2=dT2*e2 :rC=dC*e2: rM=dM*e2 :if Nd>0 or Myd>0 then rM=diam*e2

ba=bw:if bw=0 then hf=h :ba=b '

bb=esca*b : hh=esca*h '

rr=rec*esca '

incre=0.015*esca-rT:rr1=rr+incre '

hff=esca*hf: qq=hh-hff: bww=esca*ba: bwE=bww-2*rr '

bwE1=bww-2*rr1 '

ala1=(b-bw)/2 : ala=(bb-bww)/2 '

d.i=(w.w-bb)/2 : d.s=(w.h-hh)/2 '

w.h=25+25+hh '

di=d.i+rr: ds=w.h-rr: bE=bb-2*rr: hE=hh-2*rr '

di1=d.i+rr1 : bE1=bb-2*rr1 '

'---------------------------------------------------

#g "color blue ; size 1"

#g "backcolor blue"

'--------------------------

if len(COdA$)<3 then

ndv=8:x(1)=ala1:y(1)=0:x(2)=ala1:y(2)=h-hf:x(3)=0:y(3)=h-

hf:x(4)=0:y(4)=h:x(5)=b:y(5)=h

x(6)=b :y(6)=h-hf:x(7)=ala1+bw:y(7)=h-hf :x(8)=ala1+bw:y(8)=0

:x(9)=ala1:y(9)=0

end if

'..................................

if desplaza=0 and len(COdA$)>2 then

for n=1 to ndv+1

x(n) =x(n) +xMIN*sgn(xMIN)

xs(n) =xs(n) +xMIN*sgn(xMIN)

xs.e2(n)=xs.e(n)

xs.e(n) =xs.e(n) +xMIN*sgn(xMIN)

xs.a(n) =xs.a(n) +xMIN*sgn(xMIN)

xs.e1(n)=xs.e1(n)+xMIN*sgn(xMIN)

next

desplaza=1

end if

'..................

for n=1 to ndv

#g "line ";d.i+x(n)*esca;" ";w.h-y(n)*esca;" ";d.i+x(n+1)*esca;" ";w.h-

y(n+1)*esca

if len(COdA$)>2 then ' en caso de ser un poligono

if val (right$(dato$(2),1))>0 then

pp=n+1: pp2=n+2: if n=ndv then pp=1:pp2=2

aa=n-1 : if n=1 then aa=ndv

xm1=x.man.p(n) *esca

ym1=y.man.p(n) *esca

xm2=x.man.a(pp) *esca

ym2=y.man.a(pp) *esca

xm3=x.man.a(pp2)*esca

ym3=y.man.a(pp2)*esca

'.....................

cc=(R+e)/R

xx=xs.a(pp):yy=ys.a(pp)

xn=xs.a(n) :yn=ys.a(n) : gosub [linea]

'.....................

cc=1

xx=xs.e(pp):yy=ys.e(pp)

xn=xs.e(n) :yn=ys.e(n) : gosub [linea]

'.....................

end if

#g "backcolor white"

#g "place ";d.i+x(n)*esca+6;" ";w.h-y(n)*esca+6: #g "\";n

#g "backcolor blue"

#g "place ";d.i+xs(n)*esca;" ";w.h-ys(n)*esca:#g "circlefilled "; rC

if N(n)>2 then 'si hay mas de dos redodos en una cara

D.x=(xs(n+1)-xs(n))/(N(n)-1) : D.y=(ys(n+1)-ys(n))/(N(n)-1) 'distancia

for m=1 to N(n)-2

#g "place ";d.i+(xs(n)+m*D.x)*esca;" ";w.h-(ys(n)+m*D.y)*esca:#g

"circlefilled "; rC

next m

end if

end if

next

if right$(dato$(2),1)="L" then

for nn=1 to 6

n(0)=1 : n(1)=2 : n(2)=3 : n(3)=4 : n(4)=5 : n(5)=6 : n(6)=1 :n(7)=2:n(8)=3

'gamma(nn)=gamma(n(nn))

'alfa(nn)=alfa(n(nn))

pp=n(nn+1)

aa=n(nn-1)

pp2=n(nn+2)

n1=n(nn)

n=n(nn)

xm1=x.man.p(n1) *esca

ym1=y.man.p(n1) *esca

xm2=x.man.a(pp) *esca

ym2=y.man.a(pp) *esca

xm3=x.man.a(pp2)*esca

ym3=y.man.a(pp2)*esca

'.....................

cc=(R+e)/R

xx=xs.a(pp) :yy=ys.a(pp)

xn=xs.a(n1) :yn=ys.a(n1) : gosub [linea]

if nn=6 then

x5=xs.e1(5) : y5=ys.e1(5)

#g "goto ";d.i+((xs.e1(4)+x5)/2+r+e)*esca;" ";w.h-((ys.e1(4)+y5)/2-R) *esca

#g "line ";d.i+((x5+xs.e1(6))/2-R) *esca;" ";w.h-((y5+ys.e1(6))/2+r+e)*esca;" ";_

d.i+ (xs.e1(2)+(R)) *esca;" ";w.h- (ys.e1(2)+(R+e)) *esca

#g "line ";d.i+ (xs.e1(2)+(R+e)) *esca;" ";w.h- (ys.e1(2)+(R+e)) *esca;" ";_

d.i+xs.e(2)*esca+xm1*cc;" ";w.h-ys.e(2)*esca-ym1*cc

'd.i+ (xs.e1(2)+(R+rec)) *esca;" ";w.h- (ys.e1(2)+(R+e)) *esca

end if

'.....................

cc=1

xx=xs.e(pp) :yy=ys.e(pp)

xn=xs.e(n1) :yn=ys.e(n1) : gosub [linea]

if nn=6 then

x5=xs.e1(5) : y5=ys.e1(5)

#g "goto ";d.i+((xs.e1(4)+x5)/2+r)*esca;" ";w.h-((ys.e1(4)+y5)/2-R)*esca 'ver

#g "line ";d.i+((x5+xs.e1(6))/2-R)*esca;" ";w.h-((y5+ys.e1(6))/2+r)*esca;" ";_ 'h

d.i+ (xs.e1(2)+R) *esca;" ";w.h- (ys.e1(2)+R) *esca

#g "line ";d.i+ (xs.e1(2)+R+e) *esca;" ";w.h- (ys.e1(2)+R) *esca;" ";_

d.i+xs.e(2)*esca+xm1*cc;" ";w.h-ys.e(2)*esca-ym1*cc

'd.i+ sm1+(xs.e1(2)) *esca;" ";w.h- (ys.e1(2)+R) *esca

end if

'.....................

next

end if

if len(COdA$)>2 then [fuera]

#g "backcolor white"

#g "place ";d.i+ala+bww/4;" ";w.h+16 :#g "\";"b = ";d0$(ba*100)

#g "place ";d.i-60;" ";w.h-(hh-xd*esca-25) : #g "\";"h= ";d0$(h*100)

'......................................................................

#g "color red ; size 1" 'linea neutra

If Myd=0 then

if xd>hf then incre=ala else incre=0

#g "line ";d.i+incre;" ";w.h-(hh-xd*esca);" ";d.i+bb-incre;" ";w.h-(hh-

xd*esca)

for n=1 to bb step 5

if n<ala or n>ala+bww then altu=hff else altu=xd*esca

if xd<hf then altu=xd*esca

#g "line ";d.i+n ;" ";w.h-(hh-altu);" ";d.i+n;" ";w.h-hh :next

#g "place ";d.i-60;" ";w.h-(hh-xd*esca) : #g "\";d2$(xd);" ";"Ln"

end if

if Myd>0 then

#g "line ";d.i+xA*esca;" ";w.h-yA*esca;" ";d.i+xB*esca;" ";w.h-yB*esca

for n=xA to b step 0.01

h.neu=yB+(yA-yB)*(xB-n)/(xB-xA) :if h.neu<0 then h.neu=0

#g "line ";d.i+n*esca;" ";w.h-h.neu*esca;" ";d.i+n*esca;" ";w.h-hh

next n

#g "place ";d.i-60;" ";w.h-(hh-Uo*esca) : #g "\";d2$(Uo);" ";"Ln"

end if

#g "color blue ; size 1"

'-----------------------------------------------------------------------------

#g, "backcolor white"

#g "place ";di+bb;" ";ds :#g "\";d0$(nT1);"r";d0$(dT)

if nT2>0 then_

#g "place ";di+bb;" ";ds-(2*rT+Dmin*10*esca/1000):#g "\";d0$(nT2);"r";d0$(dT2)

if bw>0 then_

#g "place ";di+bb;" ";ds-hE+hff-rr :#g "\";d0$(4) ;"r";d0$(dM)

#g "place ";di+bb;" ";ds-hE :#g "\";d0$(nC) ;"r";d0$(dC)

for m=2 to nBl-1 'armadura de piel

dista=(m-1)*hE/(nBl-1)

#g "place ";di+bb;" ";ds-dista :#g "\";d0$(2) ;"r";d0$(dM)

next

#g "backcolor 0 127 200"

'......................................................

#g "size 1" 'dibujo del estribo

c=0.015*esca : e=0.006*esca: a=22.5*pi/180

jose=1:if bw>0 then jose=2

for estri=1 to jose

r=rT:ala1=ala:hh1=hh:if estri=2 then ala1=0 :hh1=hff

x1=di+ala1 : y1=50+rr+(c-r)

x2=x1+bE-2*ala1: y2=y1+hh1-2*(rr+(c-r))

for p=1 to 2

e1=e*(p-1):w=c+e1

#g "place ";x1-w;" ";y1

for v=1 to 4:x=w*cos(v*a):y=w*sin(v*a):#g "goto " ;x1-x;" ";y1-y:next'su iz

for v=0 to 4:x=w*sin(v*a):y=w*cos(v*a):#g "goto " ;x2+x;" ";y1-y:next'su de

for v=0 to 4:x=w*cos(v*a):y=w*sin(v*a):#g "goto " ;x2+x;" ";y2+y:next'in de

for v=0 to 4:x=w*sin(v*a):y=w*cos(v*a):#g "goto " ;x1-x;" ";y2+y:next'in iz

#g "goto " ;x1-w;" ";y1

next

next

x1=d.i+rr+ala ' : y1=50+rr+(c-r)

x2=x1+bb-2*rr-2*ala: y2=y1+hh-2*(rr+(c-r))

if bw=0 then

pp=(c-rC)/sqr(2)

for m=1 to nC 'armadura de compresion

dista =(m-1)*(bE+2*pp)/(nC-1)

pp1=c-rC-pp:if m<>1 and m<>nC then pp1=0

#g "place ";x1-pp+dista;" ";y1-(c-rC)+pp1:#g "circlefilled "; rC

next

end if

'.........................................................

pp=(c-rT)/sqr(2)

for m=1 to nT1 'armadura de traccion

dista =(m-1)*(bE-2*ala+2*pp)/(nT1-1)

pp1=c-rT-pp:if m<>1 and m<>nT1 then pp1=0

#g "place ";x1+dista-pp;" ";ds-pp1:#g "circlefilled "; rT

next

for m=1 to nT2

dista=(m-1)*(bE-2*ala+2*(rT-rT2)+2*(c-r))/(nT2-1) 'rT-rT2

#g "place ";x1-(c-r)-(rT-rT2)+dista;" ";ds-(rT+rT2+Dmin*esca/100):_

#g "circlefilled "; rT2

next

' .....................................................................

for m=2 to nBl-1 'armadura de piel

dista=(m-1)*hE/(nBl-1)

#g "place ";x1-(c-r)-(rT-rM) ;" ";ds-dista: #g "circlefilled "; rM

#g "place ";x1+(c-r)+bwE+(rT-rM);" ";ds-dista: #g "circlefilled "; rM : next

'*********************************************************************'

if bw>0 then 'armadura de compresion en secciones en T

#g "place ";x1-ala ;" ";w.h-qq-rr+(r-rM):#g "circlefilled ";rM 'barras bajo ala

#g "place ";x2+ala ;" ";w.h-qq-rr+(r-rM):#g "circlefilled ";rM

'.........................

#g "place ";x1-ala ;" ";y1-(c-rC) : #g "circlefilled "; rC 'barras superiores

#g "place ";x1 ;" ";y1-(c-rC) : #g "circlefilled "; rC

#g "place ";x2 ;" ";y1-(c-rC) : #g "circlefilled "; rC

#g "place ";x2+ala ;" ";y1-(c-rC) : #g "circlefilled "; rC

'.....................................................

end if

[fuera]

planta=0

#g "flush"

return

'..........................

[linea]

#g "line ";d.i+xn*esca+xm1*cc;" ";w.h-yn*esca-ym1*cc;" ";_ 'linea interna

d.i+xx*esca-xm2*cc;" ";w.h-yy*esca+ym2*cc

'' if y(pp)<y(n) and x(pp+1)>x(pp) then

' #g "goto ";d.i+xx*esca+xm3*cc;" ";w.h-yy*esca -ym3*cc

'' else

if right$(dato$(2),1)="L" and nn=6 then [water]

for m=1 to 4

a=gamma(pp)+(2-m)*alfa(pp)/4

signo=sgn(y(pp)-y(n)):if y(pp)-y(n)=0 then signo=sgn(x(n)-x(pp))

if right$(dato$(2),1)="L" and (nn=5 or nn=1) then signo=-1*signo

x2=(cc*R*cos(a*pi/180))*signo

y2=(cc*R*sin(a*pi/180))*signo

#g "goto ";d.i+xs.e1(n+1)*esca+x.man(pp)*cc*esca-x2*esca;" ";_

w.h-ys.e1(n+1)*esca-y.man(pp)*cc*esca+y2*esca

next m

''end if

[water]

return

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

[310] '

if dime=3 then '

x=-1*x: xa=cr1*x-sr1*z: za=sr1*x+cr1*z'

x=cr2*xa+sr2*y : ya=cr2*y-sr2*xa '

z=cr3*za-sr3*ya: y=sr3*za+cr3*ya '

x=x+mx : y=y+my: z=z+mz '

sx=d*x/z:sy=d*y/z '

end if '

return '

'------------------------------------------------------------

[guardar.bmp] '

for n=1 to 2 :#g,"when leftButtonDown [getCoords]" :next '

WindowHeight=abs(yyy(1)-yyy(2)) '

#g "getbmp cercha "; 1;" "; 1;" ";WindowWidth;" "; WindowHeight'

bmpsave "cercha", "cercha.bmp" '

wait '

'--------------------------------------------------------------

[getCoords] '

xxx(n) = esca*MouseX : yyy(n) = esca*MouseY '

#text MouseX;" ";MouseY '

wait '

'--------------------------------------------------------------

[borrar.perspectiva] '

for n=Nba to 1 step -1 :print #g, "delsegment "; segId(n):next '

#g "redraw" '

return '

'-----------------------------------------------------------------

'oooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooo

[edText] 'Edita el texto '

prompt "TEXT>"; text$ : wait '

'+++++++ '

[adText] 'Situa texto en el dibujo '

call StopDraw '

#g "when leftButtonDown [add]" '

texto=0 : wait '

'---------------------------------------------

[add] '

dim pixel$(3000,8) '

#1.tex5, "!contents? ttto" '

texto=1 '

call SetDraw '

if lineColor$="" then lineColor$="black" '

color$=lineColor$ 'se toma el color del ultimo color de linea

alt$="white" 'se fija el color de fondo de texto blanco

size=ttto 'se toma el tamaño de texto desde #1.text5

#g "color "; color$; " ; backcolor "; alt$

#g "font ";font$;" ";str$(ttto) 'font arial 8 italic bold strikeout underscore

startX = MouseX : startY=MouseY '

'

#g "place ";MouseX; " "; MouseY '

#g "|"; text$ '

#g "flush" '

text=text+1 '

text$(text, 1)=str$(MouseX) '

text$(text, 2)=str$(MouseY) '

text$(text, 3)=color$ '

text$(text, 4)=alt$ '

text$(text, 5)="Arial" 'font$ '

text$(text, 6)=text$ '

texto=1 '

wait '

'..........................................................................

sub SetDraw 'detecta Mouse Input '

startX = MouseX : startY=MouseY '

#g, "when leftButtonDown [draw]" :#g, "when rightButtonDown [altDraw]" '

#g, "when leftButtonMove [draw]" :#g, "when rightButtonMove [altDraw]" '

end SUB '

'................

sub StopDraw 'ignora Mouse Input

#g, "when leftButtonDown" : #g, "when rightButtonDown"

#g, "when leftButtonMove" : #g, "when rightButtonMove"

end SUB

'--------------------------

[draw]

#1.tex5, "!contents? size"

pixel=pixel+1

color$="black"

pixel$(pixel, 1)=str$(size)

pixel$(pixel, 2)=color$

pixel$(pixel, 3)=str$(MouseX)

pixel$(pixel, 4)=str$(MouseY)

#g "size ";size; " ; color "; color$; " ; set ";MouseX; " ";MouseY

#g "flush"

modr=1

wait

'------------------------------

[altDraw]

#1.tex5, "!contents? size"

pixel=pixel+1

alt$="white"

pixel$(pixel, 1)=str$(size)

pixel$(pixel, 2)=alt$

pixel$(pixel, 3)=str$(MouseX)

pixel$(pixel, 4)=str$(MouseY)

#g "size "; size; " ; color "; alt$; " ; set "; MouseX; " "; MouseY

#g "flush"

modr=1

wait

'-------------------------------------------------------------------

'*******************************************************************

'-------------------------------------------------------------------

sub openGraphWindow '

if properties(0) = 0 then '

UpperLeftX=DisplayWidth/3 :WindowWidth =2*DisplayWidth/3 '

UpperLeftY=DisplayHeight*0.95*0.5:WindowHeight=DisplayHeight*0.95*0.5 '

g$="SysGraph\" '

menu #g, "&File" ,"&Nuevo" ,[nuevo] ,"&Save" ,[save], _ '

"&print" ,[printIt] ,|,"&Exit" ,[quit] '

menu #g, "&Objecto","&Linea" ,[setForLine],"&Elipse" ,[setForEllipse],_'

"&Box" ,[setForBox] ,"&Bitmap" ,[setForPan] '

menu #g, "&Colores","&Rojo" ,[colorRed] ,"&Amarillo",[colorYellow],_ '

"&Verde" ,[colorGreen],"&Azul" ,[colorBlue] '

menu #g, "&Lineas" ,"&Grueso",[lineThickness],"&Color",[lineColor] '

menu #g, "&Texto" ,"&Editar",[edText] ,"&Situar" ,[adText] '

'

bmpbutton #g, g$;"col_rojo.bmp", [colorRed] , UL, 0, 0 '

bmpbutton #g, g$;"col_amar.bmp", [colorYellow] , UL, 28, 0 '

bmpbutton #g, g$;"col_verd.bmp", [colorGreen] , UL, 56, 0 '

bmpbutton #g, g$;"col_azul.bmp", [colorBlue] , UL, 84, 0 '

bmpbutton #g, g$;"col_negr.bmp", [color.negro] , UL, 112, 0 '

bmpbutton #g, g$;"col_blan.bmp", [color.blanco] , UL, 140, 0 '

bmpbutton #g, g$;"panbttn.bmp" , [setForPan] , UL, 224, 0 '

bmpbutton #g, g$;"circbttn.bmp", [setForEllipse], UL, 252, 0 '

bmpbutton #g, g$;"sqrbttn.bmp" , [setForBox] , UL, 280, 0 '

bmpbutton #g, g$;"linebttn.bmp", [setForLine] , UL, 308, 0 '

dim tipo$(15) '

bmpbutton #g, g$;"pencil.bmp" , [lineThickness], UL, 336, 0 '

bmpbutton #g, g$;"grphbttn.bmp", [lineColor] , UL, 364, 0 '

'

open "Esquema seccion" for graphics as #g '

'**************************************** '

#g "trapclose [closeGraph]" '

#g "down" : properties(0) = 1 '

else '

WindowWidth=2*DisplayWidth/3 '

#g "cls" '

end if '

end sub '

'........ '

[closeGraph] '

call closeGraphWindow :wait '

'........ '

sub closeGraphWindow '

if properties(0) =1 then close #g : properties(0) =0 '

if properties(8) =1 then close #c : properties(8) =0 '

if properties(9) =1 then close #3d: properties(9) =0 '

if properties(11)=1 then close #3r: properties(11)=0 '

end sub '******* '

'------------------------------------------------------------

sub openTextWindow '

if properties(1)=1 then call closeTextWindow '

if properties(1) = 0 then 'solo abre si esta cerrada '

UpperLeftX=1.7*DisplayWidth/3: WindowWidth =1.3*DisplayWidth/3 '

UpperLeftY=1 : WindowHeight=DisplayHeight*0.95*0.5 '

open "Calculos de la Cercha 3D" for text as #t '

'********************************************* '

print #t, "!trapclose [closeText]"; '

properties(1) = 1 '

else '

#t "!cls"; '

end if '

end sub '

[closeText] '

call closeTextWindow '

wait '

sub closeTextWindow '

if properties(1)=1 then close #t: properties(1)=0 '

end sub '********** '

'-------------------------------------------------------

'-------------------------------------------------------

'[Mensaje] 'Mensaje de error

' #t #text, "ERROR EN "; er$

' #t #text, "ntip = ";ntip;" Nbt= ";Nbt;" "; "i= ";i;" ";"Nnu= ";Nnu;_

' " j= ";j;" Nnu= ";Nnu;" i= ";i;" j=";j;" j-i=";j-i;" Ndi= ";Ndi

' WHILE INKEY$ = "": WEND

' RETURN

'wwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwwww

function u0$(kk): u0$=using ("#",kk)

end function

function u1$(kk): u1$=using ("#.#",kk)

end function

function u2$(kk): u2$=using ("#.##",kk)

end function

function u4$(kk): u4$=using ("#.####",kk)

end function

function u6$(kk): u6$=using ("#.######",kk)

end function

'-----------

function d0$(kk): d0$=using ("##",kk)

end function

function d2$(kk): d2$=using ("##.##",kk)

end function

function d3$(kk): d3$=using ("##.###",kk)

end function

function d4$(kk): d4$=using ("##.####",kk)

end function

function d5$(kk): d5$=using ("##.#####",kk)

end function

function d6$(kk): d6$=using ("##.######",kk)

end function

function d8$(kk): d8$=using ("##.########",kk)

end function

'-----------

function t0$(kk): t0$=using ("###",kk)

end function

function t1$(kk): t1$=using ("###.#",kk)

end function

function t2$(kk): t2$=using ("###.##",kk)

end function

function t3$(kk): t3$=using ("###.## #",kk)

end function

'-----------

function q0$(kk): q0$=using ("####",kk)

end function

function q1$(kk): q1$=using ("####.#",kk)

end function

function q2$(kk): q2$=using ("####.##",kk)

end function

function q3$(kk): q3$=using ("####.###",kk)

end function

'-----------

function c0$(kk): c0$=using ("#####",kk)

end function

function c1$(kk): c1$=using ("#####.#",kk)

end function

function c2$(kk): c2$=using ("#####.##",kk)

end function

function c3$(kk): c3$=using ("#####.###",kk)

end function

function c6$(kk): c6$=using ("#####.######",kk)

end function

'-----------

function v0$(kk): v0$=using ("#######",kk)

end function

function v2$(kk): v2$=using ("#######.##",kk)

end function

function v3$(kk): v3$=using ("#######.###",kk)

end function

'-----------

function s1$(kk): s1$=using ("######.#",kk)

end function

'--------------------------------------------------

function eee$(ee) '

n1$ = using ("######################",ee) '

nn=val(left$ (n1$,4)) '

nn$=str$(nn/100) '

'if ee>0 then '

eee$= " "+nn$+"e"+str$(len(n1$)-2) '

'if ee<0 then eee$="-"+nn$+"e"+str$(len(n1$)-2) '

p=7-len(eee$) '

eee$=space$(p)+eee$ '

end function '

'---------------------------------------------------

function te$(byref aa$, byref b)

if len(aa$)>=b then

te$=left$(aa$,b)

else

vacios=b-len(aa$): te$=space$(vacios)+aa$

end if

end function

'.......................................

function sgn(byref a)

if a<0 then sgn=-1

if a>0 then sgn=1

if a=0 then sgn=1

end function

'---------------------------------------------------

[formato]

if n mod nb<>0 and n<xx then #port " , ";

if n mod nb =0 or n=xx then #port ""

return

'ooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooo

[cerchas]

'********

If nombre$="" then Notice "Hay que crear una estructura primero" :wait

#1.L,"!contents? b": #1.H,"!contents? h": #1.p , "!contents? bw"

#1.t,"!contents? hf": #1.e,"!contents? fck" :#1.tipo, "!contents? tipo"

#1.nombre, "!contents? nombre$":#1.pe,"!contents? fyk":#1.UeF, "!contents? UeF$"

#1.UeL$, "!contents? UeL$": #1.re, "!contents? rec": #1.ch, "!contents? ch"

#1.ca, "!contents? ca": #1.cf, "!contents? cf"

open nombre$+".dat" for output as #cer

#cer nombre$;" Tipo=";tipo;

if tipo>100 and tipo<200 then goto [cerchas2D]

'---------------------------------------------------------------------

If tipo=201 then

end if

'oooooooooooooooo

if tipo=202 then

end if

'ooooooooooooooooo

If tipo=301 then

end if

'-----------------

if tipo=302 then

end if

close #cer

wait

'ooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooo

[cerchas2D] '*

'******** '*

'******************************************************************

if tipo=101 or tipo=102 then 'rectangular y seccion T

#cer "nombre tipo UeF UeL Md b h bw hf rec nC dC nT dT"

#cer te$(nombre$,9);" ";te$(str$(tipo),4);" ";te$(UeF$,2);" ";te$(UeL$,2);" ";_

te$(str$(Md),7);" ";te$(str$(b),4);" ";te$(str$(h),4);" ";te$(str$(bw),4);" ";_

te$(str$(hf),4);" ";te$(str$(rec),4);_ '

" ";te$(str$(nC),2);" ";te$(str$(dC),2);" ";te$(str$(nT),2);" ";te$(str$(dT),2)

end if

'---------------------------------------------------------------

if tipo=103 then

end if

'--------------------

if tipo=104 then

end if

'-----------------

close #cer

wait

'000000000000000000000000000000000000000000000000000000000000000000

[startDraw]

if texto=0 then startX=MouseX: startY=MouseY: #g "place ";startX;" ";startY

wait

'..........

[firstLine]

if texto=0 then

#g "when leftButtonMove [trackLine]"

#g "line "; startX; " "; startY; " "; MouseX; " "; MouseY

end if

oMouseY = MouseY : oMouseX = MouseX

wait

'...........

[firstFrame]

if texto=0 then

#g "when leftButtonMove [trackBox]"

#g "box "; MouseX; " "; MouseY

end if

oMouseY=MouseY:oMouseX=MouseX

wait

'.........

[trackBox]

if texto=0 then

#g "rule XOR"

#g "box " ;oMouseX;" ";oMouseY

#g "place ";startX ;" ";startY

#g "box " ;MouseX ;" ";MouseY

end if


wait

'..........

[trackLine]

if texto=0 then

#g "rule XOR"

#g "line " ;startX;" ";startY;" ";oMouseX;" ";oMouseY

#g "place ";startX;" ";startY

#g "line " ;startX;" ";startY;" "; MouseX;" "; MouseY

end if


wait

'...........

[finishLine]

if texto=0 then

#g "when leftButtonMove [firstLine]"

#g "discard;rule OVER"

#g "line ";startX;" ";startY;" ";MouseX;" ";MouseY

#g "flush ; redraw"

gosub [pepe]

end if

wait

'***********************************************

[pepe] '

n=n+1 '

#g "segment" '

input #g, segId '

#g "flush ; redraw" '

'#g "\"; segId-1 -(n-1)*2;"-";segId;" ";qqq '

#g "\"; '


m=0 '

return '

'-----------------------------------------'

[cls] '

m=m+1 '

#g "delsegment";" ";segId -(m-1)*3+1 'borra numeros

#g "delsegment";" ";segId -(m-1)*3-1 'borra lineas


qqq=qqq+3 : n=n+1 : wait '

'-----------------------------------------'

[nuevo] '

m=0 :segId=0 :n=0: qqq=2: perspectiva=0 '

#g "cls" : wait '

'-----------------------------------------'

[finishBox] '

if texto=0 then '

#g "when leftButtonMove [firstFrame]" '

#g "discard;rule OVER" '

#g "boxfilled "; MouseX; " "; MouseY '


gosub [pepe] '

end if '

wait '

'............................................................

[finishEllipse] '

if texto=0 then '



#g "place " ; int((startX+MouseX)/2); " ";int((startY+MouseY)/2) '

#g "ellipsefilled "; abs(MouseX-startX) ; " ";abs(MouseY-startY) '


gosub [pepe] '

end if '

wait '

'---------------------------------------------------

[setForLine] '

texto=0:#g "when leftButtonDown [startDraw]" '

#g "when leftButtonMove [firstLine]" '

#g "when leftButtonUp [finishLine]" '

wait '

'-------------------------------------------------

[setForBox] '



#g "when leftButtonUp [finishBox]" '

wait '

'-------------------------------------------------

[setForEllipse] '



#g "when leftButtonUp [finishEllipse]"'

wait '

'--------------------------------------------------------

[setForPan] '

texto=0:filedialog "Get *.bmp file", "bmp\*.bmp", panFile$ '

if panFile$ = "" then [inputLoop] '

loadbmp "panWithMe", panFile$ '

#g "when leftButtonDown [drawBmp]" '

#g "when leftButtonMove [MdrawBmp]" '

#g "when leftButtonUp [flushBmp]" '

wait '

'-------------------------------------------------

[drawBmp] '

#g "flush" '

#g "drawbmp panWithMe ";MouseX;" ";MouseY '

wait '

'---------------------- '

[MdrawBmp] '


#g "drawbmp panWithMe ";MouseX;" ";MouseY '

wait '

'---------------------------------------------

[flushBmp] #g "flush" :wait '

[colorRed] #g "backcolor red" :wait '

[colorYellow] #g "backcolor yellow" :wait '

[colorGreen] #g "backcolor green" :wait '

[colorBlue] #g "backcolor blue" :wait '

[color.negro] #g "backcolor black" :wait '

[color.blanco] #g "backcolor white" :wait '

'-------------------------------------------------------------------------

[lineas] '

data 15,"1","2","3","4","5","6","7","8","9","10","11","12","13","14","15" '

[colores] '

Data 13,"black","darkpink","darkblue" ,"darkgreen","darkred","darkgray" '

Data "brown","darkcyan","lightgray","pink","cyan","white","red" '

'

[lineThickness] '

restore [lineas] : a$="Grueso de Linea" : gosub [comboCaja] : wait '

[lineColor] '

restore [colores]: a$="Color de Linea" : gosub [comboCaja] : wait '

'....................................................................

[comboCaja] '

if properties(10)=0 then '

properties(10)=1 '

for n=1 to 15:tipo$(n)="": next '

read ndd:for n=1 to ndd:read c$:tipo$(n)=c$: next '

WindowWidth=210:WindowHeight=100:UpperLeftX=158:UpperLeftY=490'

combobox #col.sel, tipo$() ,[Selec] , 10,10,120,300 '

button #col.default, "Okay" ,[new] ,UL,140,10, 60, 24 '

button #col.cancel , "Cancel",[closeCol] ,UL,140,40, 60, 24 '

Open a$ for dialog as #col '

'************************* '

#col "trapclose [closeCol]" '

#col.sel "select ";selec$ '

#col.sel "setfocus" '

else '

gosub [closeCol] '

end if '

return '

'...... '

[Selec] '

wait 'espera hasta pulsar OKAY '

'......... '

[closeCol] '

if properties(10)=1 then close #col :properties(10)=0 '

wait '

'.... '

[new] '

#col.sel "selection? selec$" '

if a$="Grueso de Linea" then #g "size "; selec$ '

if a$="Color de Linea" then #g "color ";selec$ '

if left$(a$,6)="ELEGIR" then [nuevaCercha] '

wait '

'...............................................'

[nuevaCercha] '

for n=1 to ndd '

if selec$= tipo$(n) then '

tipo=tip+n: aaa$=aa$+left$(tipo$(n),12) '

gosub [do]: wait '

end if '

next '

wait '

'xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

[secciones] '

Data 4,"Rectangular","SeccionTe","Exagonal","SeccionL" '

'..............................................'

[Flexion.Simple] '

aa$="" : tip=100 '

restore [secciones]: a$="ELEGIR SECCION": gosub [comboCaja] '


UpperLeftX=DisplayWidth/3: WindowWidth =2*DisplayWidth/3 '

UpperLeftY=1 : WindowHeight=DisplayHeight*0.95 '

open "modelos de seccion" for graphics as #c '

'****************************************** '

#c "trapclose [closeGraph]" '

#c "down" : properties(8) = 1 '

loadbmp "c",g$+tipo$(1)+".bmp":#c "drawbmp c -20 0" '

loadbmp "c",g$+tipo$(2)+".bmp":#c "drawbmp c 0 215" '



#c "flush" '

end if '

wait '

'ñññññññññññññññññññññññññññññññññññññññññññññññññññññññ

[Seccion.T] '

dime=3 :rig=0 :aa$="A3" : tip=200 '

'restore [cercha.3D]: a$="ELEGIR CERCHA 3D": gosub [comboCaja]'




open "modelos de cercha3D" for graphics as #3d '

'********************************************* '

#3d "trapclose [closeGraph]" '

#3d "down" : properties(9) = 1 '

loadbmp "c",g$+tipo$(1)+".bmp":#3d "drawbmp c 0 0" '



#3d "flush" '

end if '

wait '

'ññññññññññññññññññññññññññññññññññññññññññññññññññññññ

[portico.3D] '

data 3,"cupula_pechinas","triangulo_doble" '

'...........................................................'

[PortTipo3D] '

dime=3 :rig=1 :aa$="R3" : tip=300 '

restore [portico.3D]: a$="ELEGIR PORTICO 3D": gosub [comboCaja] '




open "modelos de porticos3D" for graphics as #3r '

'********************************************* '

#3r "trapclose [closeGraph]" '

#3r "down" : properties(11) = 1 '

loadbmp "c",g$+tipo$(1)+".bmp":#3r "drawbmp c 0 0" '

loadbmp "c",g$+tipo$(2)+".bmp":#3r "drawbmp c 0 260" '

#3r "flush" '

end if '

wait '

'ñññññññññññññññññññññññññññññññññññññññññññññññññññññññññññ

[do] '

CeL=1 : gosub [unidades.entrada] '

gosub [cabecera] '

L=40/CeL ' Ancho cm '

H=25/CeL ' altura cm '

p=0:t=0: if tipo=102 then p=15 :t=20 ' secciones en T '

Md=50000 ' cmkp '

rec=4 ' cm '

ch=1.5 : ca=1.1 : cf=1.6 ' coeficientes de seguridad '

fck=175 :UeF$="kp" :UeL$="cm" ' resistencia del hormigon kg/cm2 '

fyk=4100 ' resistencia del acero kg/cm2 '

nC=2 : dC=10: nT=2 : dT=10 ' armaduras iniciales '

r1=35: r2=5 : r3=10: mx=1 : my=1 :mz=350 :kk=1 '

#1.r1 r1: #1.r2 r2: #1.r3 r3: #1.mx mx: #1.my my: #1.mz mz:#1.kk kk '

nombre$=aaa$: escala=1 '

#1.tipo tipo: #1.L L:#1.H H:#1.p p:#1.t t :#1.UeL UeL$:#1.UeF UeF$ '

#1.e fck:#1.pe fyk:#1.nombre nombre$: #1.esca escala : #1.Md Md '

#1.re rec:#1.ch ch:#1.ca ca:#1.cf cf:#1.nC nC: #1.dC dC:#1.nT nT:#1.dT dT '

gosub [closeCol] '

return '

'..............................................................................

[cabecera] '

if bw=0 then #1.x3 "Secc Rectangular"+chr$(13)+chr$(10)+"base Alt " '

if bw>0 then #1.x3 " Seccion en T" +chr$(13)+chr$(10)+"base Alt bw hf"

#1.x3 "!Disable":#1.x3 "!font arial 8 16" '

return '

'------------------------------------------------------------------------------

[save]

filedialog "Save Drawing As","*.bmp",saveFile$

if saveFile$="" then wait

if startX<oMouseX then x1=startX:x2=oMouseX else x1=oMouseX:x2=startX

if startY<oMouseY then y1=startY:y2=oMouseY else y1=oMouseY:y2=startY

#g "delsegment";" ";segId-1

#g "redraw"

#g "getbmp saver ";x1;" ";y1;" ";x2-x1;" ";y2-y1

bmpsave "saver",saveFile$

unloadbmp "saver"

#g "color blue"

segId=0

wait

'-------------------------------

[printIt] #g "print vga" :wait

[quit] call closeGraphWindow :wait

'--------------------------------

[about]

WindowWidth = 250

WindowHeight= 230

UpperLeftX=int((DisplayWidth-WindowWidth)/2)

UpperLeftY=int((DisplayHeight-WindowHeight)/2)

TexteditorColor$ ="darkblue"

ForegroundColor$ ="cyan"

aboutMessage$= programa$ +chr$(13)+chr$(13)+_

" Programa redactado por " +chr$(13)+_

" Antonio Martinez Gimenez" +chr$(13)+_

" http:\arquitectur.blogspot.com" +chr$(13)+_

" ------------------------------" +chr$(13)+chr$(13)+_

"Calculo/comprobacion de secciones"+chr$(13)+_

"de hormigon armado, rectangulares"+chr$(13)+_

"o de seccion T, a flexion simple,"+chr$(13)+_

"compuesta o esviada." +chr$(13)+_

"El programa permite introducir" +chr$(13)+_

"armadura comprimida prefijada" +chr$(13)+_

"por motivo constructivo o cal-" +chr$(13)+_

"cular su valor minimo necesario," +chr$(13)+_

"segun el momento flector." +chr$(13)+_

"La comprobacion de flexion com." +chr$(13)+_

"puede hacerse por Mom. o Carga." +chr$(13)+_

"(Cartagena/2013)" +chr$(13)+_

""

texteditor #ab.tx , 10, 10,220,160

button #ab.okBut,"OK",[ok],UL,90,175, 40, 20

if properties(7)=0 then open "CERCHAS-3D" for dialog as #ab

properties(7) =1

#ab "font ms_sans_serif 10"

#ab "trapclose [ok]"

#ab.tx, aboutMessage$

#ab.tx "!origin 1 1"

wait

'------------------

[ok] if properties(7)=1 then close #ab : properties(7)=0 : wait

Documents

flexo_compresion_v16