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Characteristics of propeller noise on an aircraft fuselage related to interior noise transmissionExterior noise was measured on the fuselage of a twin-engine, light aircraft at four values of engine rpm in ground static tests and at forward speeds up to 36 m/s in taxi tests. Propeller noise levels, spectra, and correlations were determined using a horizontal array of seven flush-mounted microphones and a vertical array of four flush-mounted microphones in the propeller plane. The measured levels and spectra are compared with predictions based on empirical and analytical methods for static and taxi conditions. Trace wavelengths of the propeller noise field, obtained from point-to-point correlations, are compared with the aircraft sidewall structural dimensions, and some analytical results are presented that suggest the sensitivity of interior noise transmission to variations of the propeller noise characteristics.
Document ID
19790042919
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mixson, J. S.
(NASA Langley Research Center Hampton, VA, United States)
Barton, C. K.
(NASA Langley Research Center Hampton, Va., United States)
Piersol, A. G.
(NASA Langley Research Center Hampton, VA, United States)
Wilby, J. F.
(Bolt Beranek and Newman, Inc. Canoga Park, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 79-0646
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aeroacoustics Conference
Location: Seattle, WA
Start Date: March 12, 1979
End Date: March 14, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A26932
Distribution Limits
Public
Copyright
Other

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