plastemartjobs.com Email: jobs@plastemart.com, hr@plastemart.com Download Date: 5/11/2025 10:00:10 PM ________________________________________________________________________________________ RefNo: CA - 32384 Gender: Male Age: 40 Designation: Senior CAE Analyst Highest Education Level: Graduate - Degree Education Details: Bachelor of Technology in Aeronautical Engineering The Indian Institute of Aeronautical Engineering & Technology, Kolhapur July 2009 Aggregate Percentage 64.05% Skill Sets: FEA SoftwAres: RADIOSS Optistruct,Ls Dyna, Abaqus, Nastran, Hypermesh Others: MS Office. Work Experience: 16.5 Work Experience Details: Senior CAE Analyst February 2016 Till date Company profile - Products are designed, engineered and manufactured. Job profile - Performed Crash analysis using LS Dyna, and Hypermesh. Performed FE modeling and connection of assemblies of various types of 1st,2nd,3rd row seats. Performed Misuse test for seat plastic parts. Correlation of physical testing and predict failure. Performed Frontal and Rear crash on 2nd row seat as per European Standard. Predict failure in seat structure and simulated design iteration for test compliance. Performed armrest loading as per requirement. Performed correlation of fea result with physical testing. Performed NVH modelling and modal analysis using Obstructionist, Nastran and Hypermesh. Performed FE modeling and connections of assemblies of various types of 1st,2nd,3rd row seats. Mass balancing for FE parts as per Bill of material, and wherever lumped masses required applied on COFG. Performed connection of assembly with different types of Welds as per customer requirement and modeling guidelines of different OEM. Correlated fea and physical results. Performed Modal and FRF analysis. CAE Analyst From December 2013 2016 January Company profile - Manufacturers of spares for thermal power plant. Job profile - Performed Various Crash analysis using LS Dyna, Radioss and Hypermesh. Knowledge of Regulations governing Automotive Safety regulations. (FMVSS, ECE-NCAP). Worked on full vehicle Frontal impact ,Side impact and Rear impact ,Roof Crush. Building High fidelity CAE Full vehicle model for test Correlation Comparison of Acceleration pulse between CAE and Test analysis Optimized Modeling approach of front end parts to correlate Test Results Understanding of Automotive crash sensors ,its response and sensitivity. Compared the CAE results with physical test. CAE Analyst nODE ELEMENT CONSULTANCY PVT LTD Pune, Maharashtra, INDIA November 2011 October 2012 Hypermesh; LS Dyna FEA; Design; Automotive Components Team Lead Planning of work and distributing of work among team members. Responsible for engineering deliverables like analysis results and data, reports and presentations. Working with team and handling deliveries, which involved frequent work delegation and out-sourcing. Performed Door forming analysis using Ls Dyna and Hypermesh. Analyzed structural analysis of ship mounted dumbbell stand analysis using Ls Dyna (Implicit) and Hypermesh. CAE Analyst (Independent Consultant) Introtech India PVT LTD Pune, Maharashtra, INDIA June 2010 October 2011 Hypermesh; LS Dyna ; Abaqus FEA; Design; Automotive Components Performed crash analysis of Front/ Rear Bumper System of passenger vehicles using Ls Dyna and Hypermesh Performed non linear static firm feel analysis using Hyper mesh and Abaqus Performed shell meshing of the Seating system, Bumper System, Car Door, IP and different automotive parts, bumper beam, bumper fascia, Rail Attachment Brackets and Crush Cans, Grille. Performed FE modeling of various Bumper foams Performed FE modeling of various plastic component with required thickness transition Performed FE modeling of various BIW Component following quality parameter for crash analysis. trainee Engineer AT Technologies Pvt. Ltd. Pune, Maharashtra, INDIA Aug 2009 June2010 Hypermesh; Nastran; FEA; Design; Automotive Components; Technical Documentation Helicopter skid landing gear dynamic drop simulation using LS-DYNA Performed Finite element validation and stress analysis results verification of commercial aircraft mid-wing section Performed FE modeling of Heavy engineering component Hoist Crane, pipe joint assembly. Performed non-linear material analysis of Cowl Flap structure to evaluate stresses on lug Performed Light Commercial Chassis and road load stress analysis ________________________________________________________________________________________