Calculation of induced efficiency of heavily loaded propellers having infinite number of blades; Induced efficiency of optimum propellers having finite number of blades; Prospects of propeller drive for high flying speeds.

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Bibliographic Details
Online Access:	Full Text (via ProQuest)
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1939.
Subjects:	Mathematical models. Aeronautics > Research. Airplanes. Aerodynamics.

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Full Text (via ProQuest)

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Call Number:	Y3.N21_5..8_884
Y3.N21_5..8_884	Available