<P> To achieve the extra lift, the lift coefficient, and so the angle of attack, will have to be higher than it would be in straight and level flight at the same speed . Therefore, given that the stall always occurs at the same critical angle of attack, by increasing the load factor (e.g., by tightening the turn) such critical angle--and the stall--will be reached with the airspeed remaining well above the normal stall speed, that is: </P> <Dl> <Dd> V s t = V s n (\ displaystyle V_ (st) = V_ (s) (\ sqrt (n))) </Dd> </Dl> <Dd> V s t = V s n (\ displaystyle V_ (st) = V_ (s) (\ sqrt (n))) </Dd> <Dl> <Dd> V s t (\ displaystyle V_ (st)) = stall speed </Dd> <Dd> V s (\ displaystyle V_ (s)) = stall speed of the aircraft in straight, level flight </Dd> <Dd> n (\ displaystyle n) = load factor </Dd> </Dl>

Which type of stall has the largest associated angle of attack