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Prakash_Resume_Latest_Jan-17 • 1. Prakash Vaddar E-mail: Prakashmech51@gmail.com Mobile Number: +89 OBJECTIVES Seeking an innovative and competitive environment through which I can enhance my skills and Product knowledge in the field of Structural Analysis. CAREER SUMMARY  Have more than 6.0 years of experience in engineering design and analysis of Structural Components using Nastran, Patran, Hyper-mesh, Hyper-view, Optistruct and Abaqus, MDESIGN, CETIM COBRA  Determine analysis requirements, identify appropriate analysis methods and work out detailed analysis procedures to perform required analysis and evaluate the results.  Responsible for execution and successful delivery of the FEA meshing and analysis projects, meeting customer's time line and quality requirements.  Have good experience in linear static analysis, modal Analysis, Dynamic Analysis, Material and geometric non-linear and Non-linear Contact Analysis  Good Working knowledge on Metallic, Composite laminates and Plastic structural Components.  Sound knowledge of validation of bolted joints under static and fatigue loading conditions by using MDESGN and CETIM COBRA.  Hand calculations (Lug analysis, Bolt stress, & Joint analysis) to support and validate the analysis results.

 Documenting and preparing stress reports for all the analyzed components. Prepared more than 100 stress reports which are approved by FAA.  Have H1B visa valid till April 2018. KEY SKILLS Technical Skills Summary: Pre Processor: Hypermesh, Simlab, Ansa Solvers: MSC Nastran, Abaqus, NX Nastran, Optistruct Post Processor: Hyperview, Abaqus, Patran Bolt calculation tools: Mdesign, CETIM Cobra, VDI-2230 CAD Tools: Catia V5, Auto CAD PROFESSIONAL CREDENTALS  Bachelor of Engineering in Mechanical Engineering, from VTU University, Belgaum. • Prakash Vaddar E-mail: Prakashmech51@gmail.com Mobile Number: +89 PROFESSIONAL EXPERIENCE • Presently working as Technical Lead in CYIENT from 07-March-2016 to till date. • Worked as Senior Analysis Engineer in AXISCADES from February 2014 to February 2016.

• Worked as senior Analysis Engineer in CYIENT(Formerly known as Infotech Enterprises Ltd) From July 2011 to Feb 2014 • Worked as a Contract Engineer in Aeronautical Development Agency from August 2010 to July 2011 • Worked as Graduate Engineer Trainee in Suzlon Energy Ltd, From November 2009 to June 2010 Projects Handled: Project: Structural Validation and Stiffness calculation of Lifter Assembly for C9 engine. Company: AXISCADES Client: CATERPILLAR, USA FEA Tools: Hypermesh, Simlab, Abaqus Team Size: 2 Project Details: • Objective of this task is to analyze and identify the stiffness of lifter assembly by applying assembly and operation loading conditions. • Detailed FE model of lifter assembly is generated by using Hypermesh. • Contacts, loads and boundary conditions are applied as specified by using Hypermesh.

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• Assembly loading condition (Interference analysis) has been performed and evaluated the stresses at the interference locations. • After assembly loading condition, the model has been verified for operational loading condition by applying valve lifting loads. The deflection obtained from this analysis is used to calculate the stiffness of the assembly.

• Prepared detailed report and evaluated with customer. Project: Bolt validation of Bogie frame bolted joints. Company: CYIENT Client: Bombardier, UK FEA Tools: Hypermesh, Nastran, MDESIGN Team Size: 1 Project Details: • Objective of this task is to evaluate the bogie frame bolted joints by using MDESGN (VDI-2230) • The bolt forces acting at the bolted joints were extracted by using hand calculations. • The bolted joint parameters required for the validation are arrived based upon the VDI-2230 • By using static and fatigue loads, the bolted joints are evaluated for Bolt Slip, Bolt Shear, Bolt yielding and contact pressure between different interfaces.

• Design change suggestions are given for bolts which are not meeting the acceptance criteria. • Prakash Vaddar E-mail: Prakashmech51@gmail.com Mobile Number: +89 Project: Flapper Press-Fit Analysis Company: AXISCADES Client: Montaplast, USA FEA Tools: Hypermesh, Abaqus. Team Size: 1 Project Details: • To find the structural integrity of the flapper for given maximum press- fit condition and torque load • Detailed FE model of lifter assembly is generated by using Hypermesh. • Contacts, loads and boundary conditions are applied as specified by using Hypermesh. • Assembly loading condition (Interference analysis) has been performed and evaluated the stresses at the interference locations. • Prepared detailed report and evaluated with customer. Project: Structural validation of Radiator Fan Mounting assembly under fatigue loads.