Vinayaka B. T.

Dynamic aerospace engineer with extensive experience at AXISCADES Technologies Limited, specializing in static strength analysis and repair justification. Proven ability to deliver technical solutions while ensuring compliance with certification standards. Strong critical thinking and effective communication skills drive successful project outcomes and foster team collaboration.

• Attended a 2-week training on 'Stress analysis of the A350 rear spar and attachments' at Cyient Limited
• Attended a 2-week training on 'Stress analysis of nacelle structure using hand calculations' at Cyient Limited
• Attended training on 'Basics of airframe structures, static and fatigue analysis, using MSC.Nastran/Patran' at BAIL, Bangalore

• Kannada, English, Hindi

Team member and leading run scorer of the winning team that won the System Analysis League Cup in 2015 at CYIENT, winner of Doubles Carrom in PW championship, Carrom Doubles winner of PW Championship 2019 at CYIENT Limited. Playing carrom and cricket are my hobbies.

A400M Center wing box and Rudder Concessions, AIRBUS, Check the strength of the component in the presence of nonconformity., Finding the nominal RF from the stress reports and calculating concession RF as per AIRBUS standards., Static and fatigue analysis are performed using Hand calculation/ISAMI., Documentation of concession reports in-line with AIRBUS standards., Complete responsibility of the package., Stress and fatigue analysis of TRAS and TS fitting, Collins Aerospace, Check the margin of safety of the components for different loading scenarios for certification., Static and fatigue analysis performed using FEM/Hand calculation., Material allowable, SN curve taken from MMPDS., Strength check, joints, lug analysis and fatigue damage calculation done by hand calculation., Margin of safety calculated in each analysis., Analysis report preparation., Engine Dynamics and Loads analysis of PW1100G and PW1400G engines, Pratt & Whitney America, Find critical speed of rotors, loads and deflections extraction at interface locations of gas turbine engines at different flight conditions., ARDA modeling of the engine components., Perform full engine IFEM validation., Perform rotor dynamics analysis to find critical speed of rotors and critical loads and deflections at different interface locations., Analysis report preparation., Stress analysis of the test rigs for SARAS rudder, RUSTOM-II fuelage, LCA midboard pylon fairing, National Aerospace Laboratories, DRDO, Design and analysis of test rigs for static strength test of aerostructures., FE modeling of the test rig, hinge brackets, attachment brackets, loading fixtures., Whiffle tree design for loading using hand calculation., Stress and deflection extraction for different components., Margin of safety calculated for different components., Analysis report preparation., Strength prediction of CFC panel under tensile load, National Aerospace Laboratories, Find the tensile strength of the 16 layer undamaged and damaged CFC panel., FE modeling of the 16 layer undamaged and damaged CFC panel., Failure load of CFC panel predicted under tensile load using first ply failure theory and Tsai-hill failure criteria., Validated with physical test., Analysis report preparation., Buckling analysis of the laminated composite plate, National Aerospace Laboratories, Find the buckling strength of the 6 layer CFC panel., FE modeling of the 6 layer CFC plate., Failure predicted using Eigen value., Effect of aspect ratio, ply orientation and multiple cut-out on the buckling studied., Analysis report preparation. STRESS ANALYSIS AND FATIGUE LIFE PREDICTION FOR STIFFENED PANEL OF THE TRANSPORT AIRCRAFT WING BOTTOM SKIN, FEM and Fatigue, MSC.Nastran/Patran, BAIL, Bengaluru, The stress analysis of the panel is done by the finite element method using software package MSC.Patran/Nastran. By this the high tensile stress location which leads to the crack to initiate is identified. Fatigue life prediction for crack to initiate is done by using S-N curve based Miner's rule. OPTIMIZATION OF RAW MATERIAL MIX FOR METAL CASTING USING LINEAR PROGRAMMING, Operational Research, GIPALS, Sri Shiva Sai Cast Pvt.Ltd, Shivamogga, The Optimization of raw material mix for metal casting is done and this is achieved by the Linear Programming method. This project helps the casting industry to obtain an optimum quantity of raw material for metal casting and hence avoid the excess material being used for a particular grade. This in turn helps the industry to avoid excess use of costly raw materials and helps in saving money.

• J2989096
• U2930439
• Father's Name: C. Thirthalingappa
• Date of Birth: 03/26/89
• Gender: Male
• Marital Status: Married