1. OBJECTIVE
A challenging career in the field of engineering within the aerospace industry and to secure a worthy position
in the group which will give the opportunity to contribute the best of my skills that can add to the overall
development of the group and at the same time improve my professional skills and ability, while being
resourceful
BRIEF OVERVIEW
 Excellent knowledge of Airplane Performance, Stability & Control
 Excellent knowledge of Aero Engine
 Basic knowledge of MATLAB
 Good knowledge and fundamental of CAE tools like ANSYS and have hands on experience in MS
Excel
 Hands on experience in static stress analysis of Aero structure components (metallic)
 Strong team contributor; consistent and reliable
 Experienced and capable of working in a diverse work force, Detail oriented, flexible and adaptable
 Willing to go the extra mile to meet team goals and deadlines
ANALYSIS SKILLS
 Stress Analysis by FE and classical hand calculation
 Structural design analysis of Aircraft airframe structures (Metallic)
 Finite Element modeling and Validation of FE modeling
TECHNICAL SKILLS
 Modeling Package: NX UNIGRAPHICS 7.5,8.5
 FEA Packages: HYPERMESH & ANSYS APDL
 Types of Analysis done: Linear Static
 MATLAB, MS OFFICE
WORK EXPERIENCE
 Worked as Graduate Engineer Trainee in GAS TURBINE RESEARCH
ESTABLISHMENT(GTRE), DRDO
Designation: Graduate Engineer Trainee
Total Exp: July 2015 to June 2016
YOGESH SAINI
Contact No-: +91-9538138640
Email -: yogi111.aero@gmail.com

2. PROJECTDETAILS
1) Feasibility study of casing
 Modeling of different casing with different configuration & specification
 Creation of FEM model in HYPERMESH
 Preprocessing & Post processing in ANSYS APDL
 Study of casing behavior
 Study of combined casing behavior
 Calculation of reserve factor of casing
 Validate FEM result from hand calculation
Tools: NX Unigraphics 8.5, Hypermesh, Ansys
2) Pressure vessel analysis
 Modeling of STFE outer casing & oxidizer tank by CAD tools
 Theoretical validation of model for analysis
 Creation of FEM modal in HYPERMESH
 Preprocessing & Post processing in ANSYS APDL
 Study of axisymmetric behavior of both casing and tank
 Calculate reserve factor for different material condition
 Documentation of analysis
Tools: NX Unigraphics 8.5, Hypermesh, Ansys
3) Component design of Small Turbofan Engine
 Modelling of engine components using CAD tools and optimization as per the specifications
 Design of Engine test rig
 Design of connector, gear, connection shaft, engine attachment
 Design of Impeller, Fan blisk, HPC&LPC disk & blades
 Design of turbine shaft and assembly, HPT & LPT blade
 Design of combustion chamber
Tools: NX Unigraphics 8.5
ACADEMIC PROJECT
 Study of Shock waves & types of Shock waves
 Variation of properties across the Shock waves
EDUCATION
 B.E. (Aeronautical Engineering) from The Aeronautical Society of India, DELHI
 Qualified GATE-2014 in Aerospace Engineering with AIR 164
DECLARATION
I hereby declare that the above particulars are true and correct to the best of my knowledge and belief.
Place: Bangalore YOGESH SAINI