don't think so. I am much more inclined to cut out of the discussion. I am getting tired of expounding basic aerodynamics and being told it's all wrong.
stalls, as mentioned before, can occur in any attitude, at any thrust setting and at any airspeed
--- also maximum loading is placed upon the wing at the stall,... that maximum loading varies with airspeed,
A stall at Va results in a limit load
and a stall above Va will usually result in structural failure due to ultimate loads!!!
Edit: so, therefore the AoA of the stall remains constant...
