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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
Presentation
Authors
N N Reddy (Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: Fourth Aircraft Interior Noise Workshop
Publisher: National Aeronautics and Space Administration
Volume: NASA-CP-10103
Subject Category
Acoustics
Meeting Information
Meeting: Fourth Aircraft Interior Noise Workshop
Location: Friedrichshafen
Country: DE
Start Date: May 19, 1992
End Date: May 20, 1992
Sponsors: Society of Automotive Engineers International, German Aerospace Center, National Aeronautics and Space Administration
Accession Number
92N32949
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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