Noise survey of a full-scale supersonic turbine-driven propeller under static conditions / Max C. Kurbjun.

Overall sound-pressure levels and frequency spectra of the noise emitted from a full-scale, 7.2-foot-diameter, 3, 500 rpm, three-blade, supersonic propeller mounted on a turbine-powered airplane have been obtained under static conditions at stations about the propeller at a 100-foot radius.

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Bibliographic Details
Main Author: Kurbjun, Max C.
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1957]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 4059.
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Call Number: Y 3.N 21/5:6/4059
Y 3.N 21/5:6/4059 Available Place a Hold