Engineer II, Structural Analysis (R5166)

Job description

Job responsibilities

• Assist in building and refining finite element models (FEM) to evaluate the structural performance of UAV components.
• Perform static, modal, fatigue, and vibration analyses to assess stress, deformation, and durability.
• Conduct hand calculations to validate FEA results, ensuring accuracy and structural reliability.
• Work with design engineers to optimize airframe structures, balancing weight, strength, and manufacturability.
• Support the development of test plans for structural validation, including quasi-static, vibration, and shock testing.
• Analyze flight telemetry and structural test data to improve modeling accuracy and correlate predictions with real-world performance.
• Assist in defining load cases, material properties, and design margins for UAV airframe and mechanical components.
• Document and present structural analysis reports and technical recommendations to engineering teams.

Job requirements

• B.S. in Mechanical Engineering, Aerospace Engineering, or related field.
• 2+ years of experience in structural analysis, finite element modeling, or aircraft loads analysis.
• Experience with FEA tools (ANSYS, NASTRAN, HyperWorks, or similar).
• Strong ability to perform hand calculations for structural strength, stability, and fatigue analysis.
• Knowledge of composite materials and lightweight aerospace structures.
• Familiarity with mechanical testing methods (static, vibration, and fatigue).
• Proficiency with data analysis tools (Excel, MATLAB, Python, or similar).
• Strong problem-solving skills, attention to detail, and ability to work in a team environment.