soo if we are flying at Vmo the maximum operating speed of aircraft and increase the maximum AOA the airflow wont increase up to Mcrit?
i was wondering that as heavy aircraft fly at its maximum cruise altitude where an aircraft reaches its maximum speed where speed cannot be increases if it were to happen the aircraft will reach to the mach and where there is a problem to be tuck under , as it reaches to the point where he can no longer increases the airspeed he will increases the AOA to compensate for the lift to weight ratio, so when he increases AOA wont the wing increases airflow to 1 mach ?
