The overall wing does not change angle if it is fixed, just these surfaces move up and down. b) For the same thrust and moving at particular speed, an increase in AOA always increases lift for an aircraft. The increased lift causes the airplane to start climbing (changing altitude) s...
“…A single erroneously high angle of attack (AOA) sensor input to the flight control system while the flaps are retracted can cause repeated airplane nose-down trim of the horizontal stabilizer and multiple flight-deck effects. These effects include stall warning acti...
or when operating in airplane it is generally believed that V-22 is capable of conducting a survivable, all engines-inoperative emergency landing, although considerable risk is incurred in such a maneuver because of the very high sink rate of V-22 and the high airspeed needed for the maneuver...
“…A single erroneously high angle of attack (AOA) sensor input to the flight control system while the flaps are retracted can cause repeated airplane nose-down trim of the horizontal stabilizer and multiple flight-deck effects. These effects include stall warning activation, airspeed disagree alert...