Originally Posted by
Airmann
Sure but an increase in speed while pitch remains constant increases the lift and thus changes the aircraft trajectory, which in turn lowers the angle of attack.
This is true, but in the end the reduction in AOA is accomplished by the stick being pushed forward, as it always is; and this must not be forgotten. (Especially in planes with underwing engines and a nose-up thrust couple.) The phrase "powering out of the stall" needs to die in a fire, starting yesterday, because people are always going to misinterpret it in the most simplistic way possible. Say "only reduce the AOA a little bit" instead.