Support loads development for propellers through rotordynamics simulations.
Correlate simulation models to wind tunnel, ground test, and flight data.
Build static and fatigue loads databases for airframe structure design.
Support aeroelastic analyses (flutter and whirl flutter) of the vehicle.
Define and develop vehicle design load cases per requirements; maintain certification docs.
Support wind tunnel and flight test planning, instrumentation, data analysis, and reports.

🎯 Requirements

MS / PhD in Aerospace Engineering or related fields
5+ years industry experience
Proven expertise in helicopter rotor aeromechanics (aero, dynamics, loads, stability, performance)
Static/dynamic loads derivation for fixed-wing and rotorcraft (rotor loads)
Experience with rotor analysis software RCAS CAMRAD II FlightLab DYMORE
Python and/or Matlab scripting

🎁 Benefits

Base pay between $182,500- $228,100
Equal Opportunity employer

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