Spin Resistant Aircraft Configuration

摘要

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.