• Develop, analyze, and own aircraft external loads across all phases of design, from early conceptual sizing through detailed certification-level substantiation. • Perform static and dynamic structural analyses, including maneuver, gust, ground, and environmental loading conditions. • Lead and execute flutter, aeroelastic stability, and structural dynamics analyses at the component and full-vehicle level. • Plan, execute, and post-process Ground Vibration Testing (GVT) and Structural Mode Interaction (SMI) testing and related modal testing, including model correlation and updating. • Support flight flutter testing, including pre-test analysis, real-time monitoring, and post-flight data interpretation. • Create and maintain finite element models for loads and dynamics applications, ensuring alignment with structural design assumptions and test results. • Develop and validate analysis methods, scripts, and tools to enable efficient, repeatable loads and aeroelastic assessments. • Collaborate closely with stress, structural design, flight test, and systems teams to ensure loads and dynamics assumptions are well understood and correctly applied.