Yeah, Shuckins had the explanation in his post:
"Early Corsairs had a serious tendency to drop their left wing abruptly during a power-on stall during landing. To correct this, Chance-Voung installed a leading edge strip, or spoiler on the right wing, just out-board of the "crank" or bend section. This caused the right and left wings to stall at approximately the same time, but also increased the stall speed. One Vought pilot is quoted in Francis Dean's AHT as stating, "I found the device had more of a psychological effect for apprehensive pilots than a positive cure for the unsymmetrical stall."
I didn't claim otherwise. I just speculated of what was the reason for such behavior from aerodynamic point of view. I may be wrong, of course -just wanted to discuss about the matter.
Does anybody know if there is any kind on built in wash-out in Corsair's wing?
-C+