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Climb to Cruise Noise Test ResultsA semi-empirical formula for the prediction of the broadband shock associated noise from rectangular supersonic jets in the fly-over plane has been developed. The predicted noise spectra compared very favorable with the measurement of Ponton, Manning and Seiner. Extension to side-line directions will be carried out.
Document ID
19990110634
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Joshi, M. C. (McDonnell-Douglas Aerospace Long Beach, CA United States)
Yamamoto, K. J. (McDonnell-Douglas Aerospace Long Beach, CA United States)
Donelson, M. J. (McDonnell-Douglas Aerospace Long Beach, CA United States)
Golub, R. A. (NASA Langley Research Center Hampton, VA United States)
Rawls, J. W. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
September 1, 1999
Publication Information
Publication: First NASA/Industry High Speed Research Program Nozzle Symposium
Subject Category
Acoustics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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