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Propeller rotation noise due to torque and thrustSound pressure of the first four harmonics of rotation from a full-scale two-blade propeller were measured and are compared with values calculated from theory. The comparison is made (1) for the space distribution with constant tip speed and (2) for fixed space angles with variable tip speed. A relation for rotation noise from an element of radius developed by Gutin is given showing the effect of number of blades on the rotation noise.
Document ID
19930081525
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Deming, Arthur F
Date Acquired
September 6, 2013
Publication Date
January 1, 1940
Report/Patent Number
NACA-TN-747
Report Number: NACA-TN-747
Accession Number
93R10815
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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