Job Title: Airframe Structural Engineer

Location: Fort Worth TX (Onsite)

Duration: Full Time

Job Description:

· Must have experience with CATIA V5/V6/3DX preferred. Other similar solid modeling CAD tools such as Pro/E, Unigraphics, SolidWorks, etc. will be considered.

· Must have working knowledge of GD&T requirements preferred.

· Must have proficiency with analytical tools or codes such as Mathcad, MATLAB, Python, Excel Visual Basic, etc. to execute custom in-house macros or results processing techniques.

· Experience working with product lifecycle management (PLM) software such as ENOVIA to drive product lifecycle.

· Previous experience working on cross functional engineering programs.

Position Requirements:

· Multiple levels of experience will be considered with at least 5 years of airframe stress analysis.

· Must have experience with NASTRAN (and visible on the resume)

· In addition, experience with at least one analysis pre/post-processor is required, including but not limited to: PATRAN, HyperWorks, Femap.

· Detailed finite element analysis (FEA) experience focused on metallic, laminated composite, castings, forgings, additive, elastomeric, or other precision components.

· Experience with computer aided design or drafting (CAD) tools in preparation of solid models for building FEM.

· Proficiency with engineering design definition including 2D/3D modeling, requirement capture, and specification development.

· Product development experience with components or systems consisting of but not limited to structural castings, precision forgings, laminated sheet, tube, or thick composites.

· Proficiency with basic office computer software, specifically the Microsoft office suite (Word, Excel, Powerpoint, Outlook, etc.).

· Demonstrated ability to work in a team environment and ability to articulate technical data and concepts to a wide audience of individuals of different technical backgrounds.

· Satisfy static strength, stiffness, stability margin, fatigue life, damage tolerance, durability, thermal performance, load distribution, failure modes and effects, and other requirements.

· Create detailed Finite Element Models (FEM) of components and assemblies using appropriate modeling practices.

· Resolve various complex structures and loading environments by applying free body diagrams, various classical analysis techniques, and other idealized models.

· Support manufacturing and testing of components and sub-systems, interpreting technical data, and assisting in product improvements.

· Review detail, assembly, and installation design definition to ensure compliance with requirements.

· Participate in a cross functional team environment completing a variety of objectives depending on the program lifecycle assigned.

· Must be able to execute tasks to program schedule and cost requirements.

· Advance the state-of-the-art through creative thought, personal and team research, technical compliance, and strong analysis skills.

· Travel to various suppliers may be expected depending on the assignment.

· Demonstrated ability to organize and prioritize a variety of activities and tasks while dealing with change.

Education Requirements:

· Bachelor's Degree in Engineering is required. Major in Mechanical or Aerospace Engineering is preferred.

· Master’s Degree in Engineering as described above is preferred.