Responsibilities:
Uses computational methods and tools in a specialized field (strength of metallic and composite structures, finite element analysis, fatigue and damage tolerance, etc.).
Responsible for establishing structural specifications and performing structural analysis on new designs of primary and secondary airframe structure.
Experience in stress analysis of subsystems and subsystems installations desired.
Required experience with structural mechanics simulation software including NASTRAN and PATRAN.
Experience using Altair HyperMesh as a pre-processor and TMP Vision for post-processing desired.
Experience with CATIA V5/3DX highly desired.
Familiarity with UNIX/LINUX operating systems.
Candidate must be capable of interpreting detail, assembly, and installation type drawings and models. Requirements:
Active Secret with investigation within 5 years or CE enrollment
Airframe primary structure layout and sizing
Hand/Excel based analysis of aerospace structures
NASTRAN and PATRAN or HyperMesh
Familiarity with Slim, Vision, and IDAT preferred
Familiarity with UNIX/LINUX operating systems preferred