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
★ Ready to Start Your European Career?
Take the next step and apply for this exciting opportunity