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New broadband shock noise model and computer code for ANOPPThe basic mechanism for broadband shock noise in supersonic jets is the interaction between the shock waves and the turbulence in the jet exhaust. This source is in addition to jet mixing noise.
Document ID
19940028983
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
April 1, 1992
Publication Information
Publication: NASA. Langley Research Center, First Annual High-Speed Research Workshop, Part 3
Subject Category
Acoustics
Accession Number
94N33489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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