Perform engineering duties such as the review of full-scale test documents, test plans, test results and test drawing. Define and validate the GFEM methodology based on available data such as displacement, interface loads and strain gauges. 2) Candidate should have an experience on GFEM modelling and basic GFEM element understanding. Knowlege on A/C load path for Fuselage, wing and Empennage is must.
Canidate should have knowledge on FEM validation, Load cases and technical concepts on acceptance FE criteria's.
Good Understanding on Aircraft loads, Boundary condition is must. Knowlege of FE tools like Hyper mesh, Nastran, Patran is a mandatory requirement.
Static, Fatigue and Damage tolerance analysis of Aero structure is an added advantage.
