The Structural Analyst is responsible for performing detailed finite element analysis (FEA) of aerospace mechanical structures subjected to static, dynamic, and thermal loads. The role involves owning analysis efforts from load definition through model creation, simulation, and reporting, with close collaboration alongside design, test, and systems engineering teams. The analyst ensures structural performance, compliance, and safety of flight hardware, subassemblies, and integrated systems under real-world loading environments.
Key Responsibilities:
Develop and execute linear and nonlinear FEA simulations to evaluate static strength, stiffness, buckling, and dynamic response (modal, shock, random vibration)
Build and validate detailed FEMs using tools such as Nastran, ANSYS, Abaqus, FEMAP, or HyperMesh
Apply aerospace-relevant load cases (e.g., pressure, thermal gradients, inertial loads, acoustic loading) based on system requirements and flight environments
Conduct margin of safety calculations using strength of materials principles and material allowables (e.g., metallics, composites)
Evaluate and document results to support design trade studies, optimization efforts, and system validation
Correlate analysis models with structural test data (vibration, static, modal) and support test planning
Interface with design, thermal, manufacturing, and test engineering teams to ensure mechanical robustness
Create detailed technical reports, analysis memos, and presentation materials for internal and customer design reviews
Support failure investigations, root cause analyses, and structural requalification as required
Contribute to process improvements, analysis templates, and standardization of modeling techniques
Key Focus Areas:
Structural FEA for aerospace systems under real-world loading conditions
Static and dynamic (modal, shock, vibration) response modeling
Analysis model creation, verification, and reporting
Interpretation of requirements, safety margins, and failure criteria
Cross-functional collaboration and engineering review participation
Qualifications & Skills:
Education:
Bachelor’s degree in Mechanical Engineering, Aerospace Engineering, or a closely related field (required)
Master’s degree in structures or applied mechanics preferred for advanced dynamic environments
Certifications:
(Not required, but the following are advantageous)
Nastran/ANSYS/Abaqus tool training or certifications
Six Sigma, DFSS, or FEA best practices courses
Experience:
3–7 years of experience in structural analysis of aerospace or high-reliability mechanical systems
Proven experience with FEA software (Nastran, Abaqus, ANSYS, HyperMesh, FEMAP, etc.)
Demonstrated ability to perform hand calculations, classical methods, and model validation
Experience with aerospace or defense hardware, including composites, bolted joints, and metallic structures
Familiarity with regulatory, qualification, and verification standards (NASA-STD-5001, MIL-STD-810, DO-160, etc.)
Technical Skills:
Strong understanding of structural mechanics, dynamics, material properties, and failure criteria
Skilled in building FEMs and interpreting complex load paths and boundary conditions
Comfortable with pre/post-processing tools and scripting (e.g., Python, MATLAB) for automation
Understanding of CAD systems and how to extract geometry for meshing (Creo, SolidWorks, CATIA)
Soft Skills:
Analytical mindset with strong technical judgment
Effective technical communication, documentation, and presentation skills
Ability to work both independently and collaboratively in a fast-paced, mission-driven environment
Attention to detail and commitment to delivering high-quality engineering deliverables