Spin recovery vs tail design
At 13:56 12 May 2009, John Smith wrote:
Nyal Williams wrote:
I've never tried this, but I have wondered whether adding downward
deflected aileron on the outside wing during a spin might 1) add drag
that
would slow the rotation, stall that wing and further reduce the
asymmetric
lift, and thus aid in stopping the spin.
Spins are aerodynamically extremely complex and each aircraft type
reacts differently.
No question; that's why it's important to read the POH.
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