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MAHESH KUMAR VANKADARI H No: 80-109E, Abbas Nagar, Kurnool, Andhra Pradesh - 518002 Phone No: +91-8971395314, E-mail:[email protected] PROFESSIONAL SYNOPSIS A competent professional with 5 years of experience in Aerospace Stress Analysis. PROFESSIONAL EXPERIENCE INFOTECH ENTERPRISES LIMITED, HYDERABAD, A.P JULY 2010 to APRIL 2014 Design Engineer Aero Euro Engineering India Pvt. Ltd, BANGALORE FEBRAUARY 2014 to Till Date Senior Design Engineer PROJECTS WORKED AT INFOTECH Project #1 A400M TED Check stress - Static Stress Analysis Client GKN Aerospace Services, UK Software used MSC Patran, MSC Nastran, MathCAD, MS-Office, AWK Summary: The scope of the project is to analyze the IFS (Inner Fixed Shroud) components and followed by extraction of loads from FEM, triggering stage 1-3 Runs using AWK scripts, preparing necessary scripts for RF Runs, preparing MathCAD according to methodology with critical loads, formatting as per customer requirement and updating of comments after HEC check and delivering the files. As of part of documentation Strength Summaries and Stress Dossiers are developed in line with Airbus Standards.

Mahesh V_Resume

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Page 1: Mahesh V_Resume

MAHESH KUMAR VANKADARIH No: 80-109E, Abbas Nagar, Kurnool, Andhra Pradesh - 518002

Phone No: +91-8971395314, E-mail:[email protected]

PROFESSIONAL SYNOPSIS

A competent professional with 5 years of experience in Aerospace Stress Analysis.

PROFESSIONAL EXPERIENCE

INFOTECH ENTERPRISES LIMITED, HYDERABAD, A.P JULY 2010 to APRIL 2014Design Engineer

Aero Euro Engineering India Pvt. Ltd, BANGALORE FEBRAUARY 2014 to Till DateSenior Design Engineer

PROJECTS WORKED AT INFOTECH

Project #1 A400M TED Check stress - Static Stress Analysis

Client GKN Aerospace Services, UK

Software used MSC Patran, MSC Nastran, MathCAD, MS-Office, AWK

Summary: The scope of the project is to analyze the IFS (Inner Fixed Shroud) components and followed by

extraction of loads from FEM, triggering stage 1-3 Runs using AWK scripts, preparing necessary scripts for RF Runs, preparing MathCAD according to methodology with critical loads, formatting as per customer requirement and updating of comments after HEC check and delivering the files. A s of part of documentation Strength Summaries and Stress Dossiers are developed in line with Airbus Standards.

Project #2 A400M Spar – Concessions and FEM Book Preparation

Client GKN Aerospace Services, UK

Software used MSC Patran, MathCAD, AWK and MS-Office

Responsibilities Concessions Preparation for A400M-Spar

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Summary: The scope of the project is to analyze the repairs like delaminating, oversize of bolt hole and

providing solution to it. As of part of documentation, concession reports are developed in line with Airbus Standards.

FEM Book preparation is to validate the FE models (Static, Dynamic and Elasto-thermal Validation). As a part of documentation a detailed report of the FEM is developed in line with the Airbus Standards.

Project #3 A350 Rear Spar – Metallic Bonded NetworkClient GKN Aerospace Services, UKSoftware used MSC Patran, MSC Nastran, MS-OfficeResponsibilities Static Stress and F & DT Analysis(Life Estimation)

Summary: The scope of the project is to prepare the stress substantiation for Static and Fatigue life estimation

of Metallic Bonding Network strips. The detail FE Modeling of the Strips is prepared for Static stress analysis to estimate the max stress. The max stress is used for the static stress calculations and as well for the fatigue life calculation. The lightning strike effects are used for the max temperature case calculation.

Project #4 Cyclic symmetric analysis of Engine Fan Blisk.Client Honda Jet, Japan

Software used Hypermesh, MSC Patran, MSC Nastran

Responsibilities FEM Model generation and Modal analysis with pre-stress and without pre-stress

Summary: The scope of the project is to do 3D Tet mesh on a single sector of Engine Fan Blisk carried out by

modal analysis (with and without pre-stress) in MSC NASTRAN and MSC PATRAN. Campbell diagram was generated to know the critical speeds.

Project #5A350XWB-900 Wingbox to Winglet Static Interface Load Reports and Stress Dossier Preparation

Client FACC,UKSoftware used MSC Patran, MSC Nastran, MS Office, ISAMI Accelerator.

ResponsibilitiesStatic Interface Loads Extraction and preparing Stress Dossier reports for the interface Components.

Summary: The scope of the project is to extract the Interface loads between Wingbox to Wingtip and Wingtip

to Winglet interfaces by using ISAMI Accelerator, and preparing the Interface load reports. Static

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Strength check is done for the interface components by using these interface loads and stress dossier reports are prepared.

PROJECTS WORKED AT AEROEURO

Project #5A350 XWB 900 MSN05 Checkstress Fatigue and Damage tolerance Analy-sis of Droop Ribs of Trailing Edge

Client GE, BangaloreSoftware used MSC Patran, MSC Nastran, MS Office, ISAMI 7.2.2.

ResponsibilitiesAnalyze the Droop Hinge Ribs critical locations and preparing Stress Dossier reports.

The scope of the project to analyze the Droop Hinge Ribs critical locations (Fillets, System bracket holes, Droop Rib to Gear Beam attachment), Upper/lower Panel strut Support Brackets, Lateral Sup -port strut Brackets, Baffle Plate & GBM system F&DT Analysis using ISAMI 7.2.2, Writing Certification Stress Report.

ACHIEVMENTS

Awarded as “Outstanding Team” for “A400M TED IFS Check stress Project”. Awarded as “Outstanding Team” for “Honda Offshore Support FEA”.

EDUCATION

G.PULLA REDDY ENGINEERING COLLEGE, KURNOOL, A.PB.Tech in Mechanical Engineering 2006- 2010

Narayana Junior College, KURNOOL, A.P12th Std 2004-2006

Ravindra Vidya Niketan, KURNOOL, A.P10th STD 2004

SKILLS

CAE software expertise : MSC PATRAN, MSC NASTRAN, ANSYS CLASSIC and HYPERMESH.Tools : Stress Dossier (Airbus), MATHCAD, ISAMI.Languages : Excel VB Script.

PERSONAL INFORMATION

Marital Status : Unmarried

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Date of Birth : 5th September, 1988Passport : YesLanguage Known : English, Telugu, and Hindi.Willing to relocate : Yes