The Loads and Aeroelasticity Engineer is responsible for the analysis and substantiation of aircraft structural loads and aeroelastic behavior to ensure safety, performance, and certification compliance. The role supports aircraft design, development, and continued airworthiness by generating and validating design loads, assessing flutter and dynamic stability, and ensuring compliance with regulatory requirements.
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Key Responsibilities
Aircraft Loads Analysis
Develop static and dynamic aircraft loads for structures, control surfaces, landing gear interfaces, and systems.
Generate internal and external loads for use in structural sizing and stress analysis.
Analyze maneuver, gust, ground, taxi, braking, and landing loads.
Support definition of design limit and ultimate loads.
Aeroelasticity & Dynamics
Perform flutter, divergence, control ...