also highly dependent on aircraft type, control loading type, danger of AOA is past a certain point
also highly dependent on aircraft type, control loading type, danger of AOA is past a certain point the wing will stall regardless of speed, at high AOA even in a PA28 during a power on stall you are pulling back hard, but of course you could trim out the control force to hold that high AOA, With the F18 Hornet they significantly increase the stick force required as AOA increases, With the Hawk a Spring is used for artificial feel but the hydraulic control system is easily capable of exceeding AOA and not to mention G's very very quickly
