Critical Angle Of Attack - [Are you sure you cannot stall at high speed?]

[@showsakovicp8783]

Thanks for your wonderful video, I am 99% percent agree with this part. But sorry, I have to say one thing, the actual situation should contain the induced flow angle so that we can get the real AOA of the airfoil. That means the relative wind is not on the flight path line, and this different create a huge factor of stall.

[@PILOTCLIMB]

Comment below your thoughts and questions!! I will help you out!! Happy Landings..

[@miltonjunior5173]

Crystal clear. The critical angle of attack creates a vortex in the upper surface of the wing, causing the airflow disconnect, so to speak. Is that it?

[@PILOTCLIMB]

Many thanks for watching and the comment! You are right!

[@Echo_Lima]

if you are in a steady climb your aoa can be zero . is that right ?

[@PILOTCLIMB]

No, it cannot be 0

[@nassoi]

can we also say its the angle between pitch attitude and flight path angle ?

[@PILOTCLIMB]

Hey, many thanks for watching!!
If you take your pitch angle and subtract the flight path angle you get the Angle of Attack.
Don't hesitate to ask any questions you might have when watching the rest of the videos I made!
I wish you a great day
Gabriele
Pilotclimb

[@bullitanaconda]

explain why jets approach to landing at a very high AOA without stalling

[@michaelmoore6777]

What language is that ?