- Minimum 10 years of experience in Stress analysis of Aero engine components using commercial Finite Element Analysis tool.
- Should have a basic knowledge in FEA Theory, Solid mechanics, Machine design and Fatigue.
- Expertise in handling various structural analysis tools preferably ANSYS Classic, Ansys Workbench, HyperMesh etc
- 2D & 3D Finite Element modeling of straightforward, moderate and complex components (Hexahedral & tetrahedral elements) using ANSYS-APDL or Workbench
- Linear and non-linear static stress analysis (Geometric, Material and contact Linearity) using ANSYS-APDL or Workbench
- Modal, Harmonic and transient Dynamic stress analysis using ANSYS-APDL or Workbench
- Strength, stability and Durability of components
- Damage tolerance analysis to estimate fracture life
- Should able to develop/modify APDL Macros
- Should able to build/update FE Models in HyperMesh.