Flight effects on subsonic jet noiseExperimental results obtained by a combination of fluid mechanics and radiated noise measurements associated with subsonic jets over a range of simulated flight speeds between 25 m/s and 110 m/s indicate that noise reduction in flight is predominantly a result of the reduced noise producing volume. These results do not support the generally accepted notion that noise reduction from jets in motion results primarily from the reduced strength of the noise producing eddies. These eddies, in flight, have previously been assumed to scale with the relative velocity V(J)-Vo where V(J) is the mean nozzle exit velocity and Vo is the flight velocity.
Document ID
19790044948
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sarohia, V. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 79-0616Report Number: AIAA PAPER 79-0616
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