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The F4U-1A Cosair
Originating in a 1938 Navy spec, when the need to replace the F2A and F4F could already be foreseen, the Vought Corsair was designed around an engine that also didn't exist yet: the Pratt & Whitney R-2800 Double Wasp, a monster 18 cylinder double radial, eventually capable of 2250 horsepower. (During the Corsair's development, corporate reorganizations brought the Vought company into Vought-Sikorsky and then Chance Vought, all part of United Aircraft, along with Pratt & Whitney and Hamilton Standard.)
The huge engine dictated much of the plane's design. Such a powerplant needed a comparably big propeller to absorb all that horsepower. Thus the 13' 4" diameter Hamilton Standard prop, the largest fittest to a fighter at that time. The Corsair's fuselage had to be high in the air, to give the prop clearance, But ordinary, straight wings at that height would have implied long (and weak) landing gear. The distinctive bent wings were developed to permit a reasonably short undercarriage.
The XF4U first flew in May 1940, and in October flew faster than 400 MPH, a record for a production fighter. A major re-design pushed the cockpit back 32 inches, which resulted in poor forward vision for the pilot, at least on take-off and landing. Development continued into 1942, when Vought delivered the first production F4U-1 to the Navy, which didn't like what it saw, especially when compared to the easier-handling, and very capable F6F Hellcat. The F4U had dangerous stall behavior, had tendency to yaw suddenly when landing, and, worst off all, bounced when it hit the deck. For use on carriers, these problems caused the Navy to insist that they be fixed, while it went ahead equipping with the Hellcat. By the summer of 1943, most of the Marine fighting squadrons had transitioned to the F4U-1, the first operational model. Based on combat experience, Vought improved the next version, the F4U-1A:
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