A configuration for an aircraft so as to be spin resistant, said aircraft comprising a fuselage and a wing wherein the wing includes a first region adjacent to the fuselage and a second region adjacent to a wing tip, the first region being contiguous with the second region, and wherein at high angles of attack a stall cell is constrained to remain within the first region so as to remain apart from flight controls within the second region.
Spin Resistant Aircraft Configuration
05.04.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |