Engineering - Structural Analysis-Stress/DADT/Dynamics/FEA/FEM



Responsible for performing stress analysis on new designs of primary and secondary airframe structure, as well as updating existing analyses to incorporate design changes. Experience with MRB stress analysis of metallic and composite structure. Required experience with FEA software including NASTRAN and PATRAN. Experience using SLIM as a pre-processor and TMP Vision for post-processing desired. Experience with CATIA V5/3DX highly desired. Familiarity with UNIX/LINUX operating systems desired. Candidate must be capable of interpreting detail, assembly, and installation type drawings and models.



Required Minimum skills:

1. Airframe primary structure layout and sizing

2. Hand/Excel based analysis of aerospace structures

3. Catia V5