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Acoustic loads prediction on jet aircraftA nearfield aircraft noise prediction computer program is presented for the F-22 aircraft. The dominant sources of noise are jet turbulent mixing noise, jet broadband shock noise, and fluctuating pressure under the turbulent boundary layer. All results from this investigation are presented in viewgraph format.
Document ID
19920023705
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reddy, N. N.
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA. Langley Research Center, Fourth Aircraft Interior Noise Workshop
Subject Category
Acoustics
Accession Number
92N32949
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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