Study of mechanical behaviour files (fatigue, progressive and excessive deformation, sudden crack) of the various materials (auxiliary lines of the main primary circuit, non-irradiated zone tanks, valves, pressurizer and steam generators, etc.) of the French Nuclear Fleet in order to free up the mechanical margins. Adoption of an input methodology on the Mechanical Margin Analysis tool (MECA margin) ensuring data homogeneity in DIPNN - TechnicalDepartment synthesis and critical analysis of the various technical documents.Elastic and elastoplastic methods used to calculate low margins using PIPESTRESS to evaluate damage such as fatigue and crack analysis. Design of internal components using NavisWorks

Executed dynamic FEM analysis on ceramics at high strain rates.Successfully designed 3D CAD models of mechanical parts using Solidworks.Designed and developed plate impact experiments using the gas launcher.

Numerical modeling of pyrotechnic spherical expansion tests.• Numerical modeling of the behavior of ceramics under confined compressive and dynamic tension loads.• Dynamic testing with plate-impact (compression), Identification of model parameters.• Numerical simulation using finite element codes.

Deformation of Metallic materials and Nickel alloys using High Pulsed Laser, sharp deformations achieved in P'Prime Labs Poitiers.• Comparative analysis of Laser Shock deformations using HYPERMESH RADIOSS• Evaluating a generalized material behavior and optimization performed using HYPERSTUDY, the trade-off between simulation and experimental results significantly low.• Reduced cost of simulation ultimately saving the cost of the company.

• Design and development Flying Wing with Jet Propulsion along with the development of the 6-DOF model on MATLAB Simulink and successfully generated control laws for the aircraft. • 3D CAD modeling using Solidworks and surface modeling using CATIA.• Lightweight and stable Airframe achieved by virtue of Structural analysis

Captain of UAV team under Creation Labs. Successfully completed design and fabrication of autonomous UAV.Structural Analysis performed, CFRP skin layed-up for High strength to weight properties