Secondary stalls
I know that a given airfoil will always stall at the same angle of attack but I'm under the impression that if you experience a 'secondary stall' then the airfoil will, in fact, stall at a lower angle of attack.
Am I incorrect?
I've looked through my books and cannot find any information. I would appreciate it if you could cite a source.
Thanks.
[Edited to ask for source]
Last edited by zerozero; 5th August 2002 at 07:08.