xxxxx
(M) : 999999999
no 0,xxx,xxx-600000
Email ID
:xxxx@gmail.com
CAREER OBJECTIVE
To be part of an Analysis group of an Engineering Industry with a good, adaptable
and motivating working environment which offers technical challenges helping me to
reach my full potential and acts as an anchor in building my career.
KEY SKILLS
 Knowledge of FE Meshing, analysis, pre and post processing

Knowledge of Airframe Design, Composite Design, Hand calculations based on Strength of
Materials approach. Experience in FE modeling using PATRAN and HyperMesh

Experience in FE analysis of primary and secondary structures using MSC
NASTRAN

Working Knowledge in 101,103 & 105 modules in MSC NASTRAN

Experience in analysis of metallic and composite structures

Experience in FE Modeling using 3D elements (Hexa, Tetra and Wedge)

Experience in preparation of Certifications reports

Experience in CAD modeling using CATIA, Solid works and AutoCAD

Working Knowledge in MS Office

Possess Good Communication skills
EXPERIENCE
1. Organization
Designation
: AERONAUTICAL DEVELOPMENT ESTABLISHMENT
: Structural Engineer
Period of Working : November 2012 – Till date
Project
: Rustom II (UAV)/ Arial Target Aircraft-ABHYAS
FEM ANALYSIS AND MODELING OF TRANSPORT JOINT
Include finding out the reaction forces at bolt locations and applying these forces in
respective locations in the conceptual FEM model. Based on the results, optimize the model
by identifying low stress regions.
Software used: Hyper Mesh, Patran, Nastran, Solid works, AutoCAD
FEM Analysis composite wing structure
Finite element modeling of wing structure using 2D elements .Linear static analysis of
carbon and glass fiber composite wing was performed. Stress and deflection values were
obtained at different locations.
Software used: HyperMesh, Patran, Nastran, MS. Excel
Weight Estimation of Composite Components
GSM method was used for weight calculation of composite components to estimate the
aircraft weight.
Software used: MS. Excel
FEM ANALYSIS OF ENGINE MOUNTING BRACKET
Engine mounting Bracket connects the engine frame to wing spars. Inertia loads were
considered.Linear static analysis was performed and Von-mises stress was obtained.
Software used: HyperMesh, Patran, Nastran, MS. Excel
DESIGN AND ANALYSIS OF 1.2m COMPOSITE WING
Wing spar design was carried out based on structural calculations.
Surface modeling of conceptual wing in CATIA
Linear static, normal modes and buckling analyses of wing were performed.
Software used: Hyper Mesh, Patran, Nastran, MS. Excel
MODIFICATION OF THE COMPOSITE WING
Wing modification is done for the structural stability on the basis of FEM analysis
Linear static analyses of wing performed
Software used: Hyper Mesh, Patran, Nastran, MS. Excel, Solid works
TESTING OF WING
Wing is testing done by using sand bags load distribution from the aerodynamics load.
Locations for the stain gauge mounting and expected results are found out by FEM analysis
Software used: Hyper Mesh, Patran, Nastran, MS. Excel
GROUND VIBRATION TESTING OF ARIAL TARGET
Ground Testing of Arial target aircraft is done using Accelerometers; Digital Signal
Processing (DSP) technology is used for data acquisition. Aircraft frequency and modes of
vibrations are studied from the data and compared with Finite element analysis results and
matched
Software used: Hyper Mesh, Patran, Nastran, MS. Excel
Roles and Responsibilities

Aircraft structural repair and maintenance.

Assisted in the setting of Structural testing.

Organized “N-SITE 2010” an Exhibition of Technical projects.
EDUCATIONAL QUALIFICATIONS
Course
Subject
University
B.E
Aeronautical
Engineering
H.S.E.
Science
S.S.L.C
-
Anna University
Chennai
Kerala state
Board
Kerala state
Board
Marks %
Class
75
First class
82
Distinction
2008
86
Distinction
2006
COMPUTER SKILLS
 Design Tools
: Solidworks, Catia V5.
 Analysis tools
: Msc Nastran & Patran, Hypermesh.
 Microsoft Office utilities : Word, Excel, PowerPoint
Personal Profile
Name
: xxxxx
Father’s Name
: xxxxx
Date of Birth
: 28th April 1991
Marital status
: Single.
Sex
: Male.
Languages known
: English, Hindi, Tamil, Malayalam
References
Will be provided on requirement.
Place
: xxxx
Date
: 05 Nov 2014
Yours truly
(xxxx)
Year of passing
2012