Towards an Aerodynamic Stall Model for the Fokker 100: A foundation for research regarding the influence of a swept wing configuration on aerodynamic stall

Research into Aerodynamic Stall Model Identification (ASMI) is an ongoing endeavor to create a model that achieves the highest fidelity, that aids in upset recovery training of pilots in Flight Simulator Training Devices (FSTD). Aircraft come in various configurations, one aircraft stall model cannot sufficiently provide a full understanding...