Sandeep Basava

**,

Tintern Crescent, Mobile No. +44-742*******

Reading, acfgbv@r.postjobfree.com

RG1 6HB

United Kingdom.

Profile

• Overall 6 years 2 month of experience in Stress Analysis in Aerospace Industry.

• Hands on experience on Aircraft Components Stress Analysis using classical hand

calculations both metallic and Composite structures.

• Worked 18 months on an onsite assignment for Airbus A400M at GKN Aerospace, UK.

• Hands on experience on FEA tools MSC Patran, MSC Nastran, Hypermesh and Ansys and

Design tool CATIA V5 R23.

Experience

• Last Employer: Tata Consultancy Services Limited.

Job Title/Role: Stress Analysis Engineer & Team Lead.

Duration: Oct 24th 2012 to 01st Aug 2014.

• Previous Employer: Infotech Enterprises Limited.

Duration: May 24th 2008 to Oct 05th 2012.

Technical Skills

Tools & Utilities MSC Nastran, MSC Patran, Hypermesh, Ansys, Catia

V5,

MS Office

Windows (98/XP/7)

Operating Systems

Education

Year of

Degree (B Tech) University Percentage/Grade

Jawaharlal Nehru Technological 76.66 (First Class with

AERONAUTICAL ENGINEERING 2008

University Distinction)

Page 1 of 4

Presentations and Conference

• Presented a paper on “The space Elevator” in a National Technical Symposium

• Attended “58th International Astronautical Congress” held in Hyderabad in September, 2007.

Personal Details

Date Of Birth 10th June 1986

Married

Marital Status

Sex Male

English, Telugu, Hindi

Languages Known

Passport No. F3780706

Projects Details

Project #1 Bombardier Global 7000/8000 Project

Client Bombardier Aerospace

Organization Tata Consultancy Services

Role/Responsibilities Analysis Engineer and Team Lead

5

Team Size

Duration 1 year 6 Months (Nov 2012 to July 2014)

MS Office, Excel VB Macros, MSC Nastran/Patran, Hypermesh, Catia V5R21.

Tools

Description Sizing of Fuselage frames in Rear Barrel using Bombardier analysis

1.

tools.

Analysis of Avionic Rack Structures using Hand calculations

2.

Building 1D and 2D FE models for Avionic Rack structures using Patran

3.

and Hypermesh.

Performing Static strength and stability checks, FE dynamic and

4.

buckling check of the Rack Structures as per Bombardier

methodologies.

Static analysis of test rig ground structures for Global 7000/8000, using

5.

hand calculations and FEA tools.

Project #2 Airbus A400M – Composite Spar Check Stress

Client GKN AEROSPACE, UK

Organization Infotech Enterprises

Role/Responsibilities Team Member and Onsite Technical Coordinator

10

Team Size

Duration 1 year 5 Months (Sept 2010 to Dec 2010 & Apr 2011 to May 2012)

Airbus analysis Tools, ESDU_93011, MSC Nastran, MSC Patran,

Tools

MS Office

Scope of the project includes analysis of Composite Spar and its attachments

Description

using Airbus analysis tools for composite analysis and preparation of Stress

Page 2 of 4

Dossier.

FEM generation from CAD models and FE analysis.

Composite Laminate Assessment, Strength Assessment of Composite Bolted

Joints and open holes.

Project #3 A400M

Client GKN Aerospace, UK.

Organization Infotech Enterprises

Tech Lead (SDE)

Role/Responsibilities

Team Size 4

9 Months (Jan 2011 to Mar 2011 & May 2012 to Oct 2012)

Duration

Tools Airbus analysis tools, MSC Patran, MSC Nastran

MS Office

Software

Description Stress Dossier write up for Spar and its attachment analyses, FEM book

generation for FE models.

Project #4 Airbus Corporate Jet 14 Program

Client Associated Air Centre, Texas.

Organization Infotech Enterprises

Team Member

Role/Responsibilities

Team Size 10

1 year 2 Months

Duration

Tools Hypermesh, MSC Patran, MSC Nastran

MS Office

Software

Description The scope of the project is to perform analysis of the interior structures using

classical hand calculation methods.

Key Steps • FE modeling of the Interior components and extracting loads for

Emergency landing, Abuse and Rapid de compression pressure.

• Performing classical hand calculations for analyzing the interior structures.

• Structural stress analysis report preparation

Project #5 Pratt & Whitney aircraft NGPF Engine Compressor Casing and Engine

Bearingss

Client Pratt & Whitney, USA.

Organization Infotech Enterprises

Role/Responsibilities Team Member

13

Team Size

Duration 8 Months

Ansys 11.0

Tools

Description The scope of the project is to analyze the casing of High Pressure Compressor

and High Pressure Turbine at various time points in the flight cycle.

Key Steps • Pre and post processing of High pressure compressor casing using Ansys.

• Considering the sub Model analysis for critical components for better

understanding of individual component behavior.

Page 3 of 4

Project #6 Post Production Engineering for 727 & 737 Fleet

Client Boeing Commercial Airplanes, Everett, USA.

Organization Infotech Enterprises

Team Member

Role/Responsibilities

Team Size 90

6 Months

Duration

Tools CSW, DTANAL, IDTAS, JOLT

MS Word

Software

Description The scope of the project includes the Damage Tolerance Assessment of repairs

in Structural Repair Manuals (SRM) and Service Bulletins (SB) of Boeing 727

and 737 airplanes. This program is to address Aging Airplane Safety Final Rule

(AASFR) to comply with FAR Part 26 rule.

Key Steps • Identifying the structural configuration of the repair location

• Selecting the configuration from CSW (Common Structures

Workstation)

• Analyzing the structure for residual strength margin

• Crack growth analysis and determining inspection threshold and

inspection intervals.

Page 4 of 4

Contact this candidate