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    Structural Analysis Engineer - Fort Worth, United States - DBSI

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    Description
    Job Role- Airframe Structural Analysis Engineer
    Job Location-Fort Worth, Texas.

    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.
    Position Responsibilities

    • 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.
    • Majoring in Mechanical or Aerospace Engineering is preferred.
    • A Master's Degree in Engineering as described above is preferred.
    #J-18808-Ljbffr


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