Noise Survey Of A Full Scale Supersonic Turbine Driven Propeller Under Static Conditions
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Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions
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.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1958
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1957