Integrates the data from all flight science disciplines to evaluate forces experienced by the aircraft on a reduced order model, treating the aircraft like a rigid body, and sometimes, when required, account for structural dynamic and aeroelastic effects Define external load envelopes representing forces summed up along a reference axis system Define external load cross-plots showing the resultant load in 2 different directions Defines the aerodynamic loads applied to the outside of any part of the aircraft exposed to airstream (air load distributions and pressure distributions based on CFD, wind tunnel and flight pressure measurements) Defines the acceleration envelope of any part of the aircraft that needs inertial loads for sizing Ensures airworthiness requirement traceability and compliance to the regulation, AKA loads database management #J-18808-Ljbffr
Loads & Dynamics Engineer
TECHDOQUEST
montreal (administrative region), montreal (administrative region)
Published 27 days ago
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