DTIC ADA380686: The Influence of Blade Width pdf

DTIC ADA380686: The Influence of Blade Width

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Description of the Book:

Combined force and wake survey tests on three-blade model propellers have been made in the Guggenheim Aeronautic Laboratory of Stanford University to determine the effects of blade-width distribution upon constant-speed efficiency characteristics. The blades of the various models differed widely in plan form but all incorporated the same pitch distribution and were of such widths as to make their activity factors equal; as a result, all the models exhibited substantially identical power-absorption capacities at equal pitch settings

• Creator/s: Defense Technical Information Center
• Date: 3/1/1949
• Year: 1949
• Book Topics/Themes: DTIC Archive, Reid, Elliot G, STANFORD UNIV CA, *AERIAL PROPELLERS, DISTRIBUTION, EFFICIENCY, PITCH(INCLINATION), SHAPE, SURVEYS, TEST AND EVALUATION, WAKE

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