Structural stress engineer - Tech M USA

Job Title: Structural Stress Engineer

Location: Red Oak, TX Day 1 Onsite at customer

JD:

What are your contributions to the team?

Perform sizing and support analysis activities for design changes, improvements, and new aircraft development programs.

Support the design process from initial concept through final production, ensuring the aircraft meets or exceeds all technical requirements

Support different teams to ensure a quality product with supporting documentation are produced.

Write structural substantiation reports, that meet technical compliance to program, and certifying authority, requirements and guidelines.

Create new and/or update existing certification DFEMs

How to thrive in this role?

You possess a B.S. in Aerospace, Mechanical or Civil Engineering from an accredited university

You have a minimum of ten (10) years of experience in aircraft structural substantiation analysis

You have a strong proficiency and experience in Fatigue and Damage Tolerance (F&DT) analysis methods and tools (i.e Nasgro)

You have a strong proficiency in classical analysis methods.

You have proficiency in FEM based analysis tools (MSC Patran/Nastran, Altair Hypermesh) developing/running DFEMs and also GFEMs (loads models)

You have knowledge of interactions between loads and structures

You have knowledge and experience of structural sizing methodologies

You have an understanding of civil aircraft certification rules and experience in certification procedures

You have excellent communication and listening skills, and the ability to interface constructively and effectively in a cross functional team environment

You must have proficiency with all Microsoft Office software applications

You have proficiency with CATIA V5, Enovia applications – preferred

You must have the ability to work on complex technical problems and provide solutions in an independent manner