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Preliminary measurements of aircraft aerodynamic noiseFlight measurements of aerodynamic noise were made on an AeroCommander airplane with engines off and a JetStar airplane with engines at both idle power and completely shut off. The overall sound level for these airplanes in the landing configuration varied as the sixth power of the aircraft velocity. For the JetStar airplane, the overall sound level decreased as the inverse square of the distance in the lateral direction. The aerodynamic noise was approximately 11 decibels below the FAR Part 36 noise level for the JetStar airplane. The landing gear were a significant contributor to aerodynamic noise for both aircraft.
Document ID
19740051582
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lasagna, P. L.
Putnam, T. W.
(NASA Flight Research Center Edwards, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
June 1, 1974
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 74-572
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Palo Alto, CA
Start Date: June 17, 1974
End Date: June 19, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A34332
Distribution Limits
Public
Copyright
Other

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