Perhaps the best way to resolve this issue is to pull out of this nosedive we're in. The F4U, while it certainly could fit, wasn't designed for carriers, while the F6F was designed for nothing but carriers.
You mean the F6F. The F4U wasn't designed for carriers. Since its first flight it had problems landing on carriers. It wasn't until after it was deployed to land then re-designed that it could even carrier-qualify for combat. I don't care what Vought imagined it designed. Are you understanding any of this? What am I missing?Where did you get THAT screwed-up idea? (the one I colored red)
The F4U was ABSOLUTELY designed for carrier use... if it had not been, then the prototype (and every example built) would not have been equipped with folding wings (powered hydraulically-operated mechanism), a tailhook (a "stinger-type" that retracted forward into the tail in the prototype, often replaced by the spin-chute dispenser for test flights, and by a normal drop-type in the production examples) and catapult bridle attachments - nor would the airframe have been designed for the stresses of arrested landings (aft half of the fuselage), the high sink rate (and hard hit) of arrested shipboard landings (landing gear support structures and wing/fuselage center sections), or the stresses of catapulted take-offs (front-center of the fuselage).
The prototype even had flotation bags in the wings, for emergency water landings (not installed in production aircraft)!