Tell ya what boys...the so-called superiority of the hog over the Jug is only evident at low altitudes. Take the Jug to 30,000 feet, where it was designed to be, and it will eat the hog alive.
According to Cokey Roberts, the Jug's low-speed stall characteristics were even better than the Hellcat's. Both of those aircraft had stall characteristics far superior to those of the Corsair. The main problem with the Jug was that when it DID stall it tended to lose a great deal of altitude before recovery, while the Hellcat did not.
The stall-tripper wedge on the hog corrected some of it's vicious stall characteristics, but also apparently hurt it's turning capability. Dean's tome "America's Hundred Thousand" rates the hog dead last of all U.S. fighters in turning capability.
Hypothetical question for those who might know...because I don't: does the dropping of flaps ALWAYS help a fighter's turning ability...or does it just lower the stalling speed? I've always assumed that it was the former...but would that be true for all aircraft?
Regards, Shuckins