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In article ,
George Ruch wrote: hobo wrote: In article , "Geoffrey Sinclair" wrote: Corsair propeller diameter 13 feet 4 inches, ground clearance 9.1 inches, engine R-2800-8. The corsair used a 3-blade prop. Why didn't they use a smaller 4-blade prop if ground clearance was such an issue? Check again, please: http://www.warbirdalley.com/f4u.htm The link you provided has no textual information regarding the prop, but there is a picture, dated 2001, of a surviving Corsair with a 4 blade prop. This prop may not be the original factory issue. When this question was first posted the first website on the Corsair I found was this: http://www.nasm.si.edu/research/aero...t/voughtf4.htm This is the Smithsonian's website and has a photo of a Corsair with a 3 bladed prop and this text: "The R-2800 radial air-cooled engine developed 1,850 horsepower and it turned a three-blade Hamilton Standard Hydromatic propeller with solid aluminum blades spanning 13 feet 1 inch." This website was my sole source for the claim that the Corsair had a 3 blade prop. Perhaps a 4 blade was later added, but it seems odd that a 3 blade was ever used if ground clearance was so pivotal to the whole design. -- |
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