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The Effect on Airplane Performance of the Factors That Must Be Considered in Applying Low-Drag Cowling to Radial Engines (1933)

NASA Technical Reports Server (NTRS) · leaf 5

An illustration from The Effect on Airplane Performance of the Factors That Must Be Considered in Applying Low-Drag Cowling to Radial Engines, 1933, leaf 5
espect to the engine and to each fuselage nose used (Navy drawing No. 3792). The diameter of this propeller had been cut from 10 feet to 9 feet. Two other fuselage nose shapes were used in Tests conducted on this propeller in the propeller- conjunction with the series of outer cowlings. The… … ETlGUBE 1.—The XF7C-1 airplane with fuselage 1 and no outer cowling (Reference 9.) The propeller pitch setting was used with an outer cowling. They are smaller in changed as the cowlings were changed, in order to diameter at the nose than the service fuselage, allowing keep the maximum engine*…

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