Stress Analysis
Resume:
Sandeep Basava
**,
Tintern Crescent, Mobile No. +44-742*******
Reading, *************@*****.***
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)
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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
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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.
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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.
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