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Effects of geometric and flow-field variables on inverted-velocity-profile coaxial jet noise and source distributionsThis paper presents relationships between the noise generation characteristics and the flow-field characteristics for inverted-velocity-profile coaxial jets. Noise measurements were made at four different sideline distances in order to determine the apparent noise source locations, and flow-field characteristics were determined from jet plume pressure/temperature surveys. These relationships are based on a published NASA Lewis prediction model, the basic assumptions of which are shown to be consistent with the experimental data reported herein. Improvements to the noise prediction procedure, on the basis of the present study, are included, which increase the accuracy of the high-frequency noise prediction.
Document ID
19790048113
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stone, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Goodykoontz, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Gutierrez, O. A.
(NASA Lewis Research Center Jet Acoustics Branch, Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 79-0635
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
79A32126
Distribution Limits
Public
Copyright
Other

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