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Propagation of plane waves in a variable area duct carrying a compressible subsonic flowA complete numerical solution is obtained for plane wave propagation in a variable-area duct which carries a mean compressible flow. The equation solved is a matrix formulation of the equations first derived by Tsien in 1952. Sample calculations are presented for four particular flow configurations: (1) a duct-nozzle-duct combination with the acoustic wave traveling with the flow, (2) a duct-nozzle-duct combination with the acoustic wave traveling against the flow, (3) an inlet-nozzle-duct configuration with the acoustic wave traveling against the flow, and (4) a duct-nozzle-exit configuration with the acoustic wave traveling with the flow. For each of these cases, the variation of energy flux with frequency is shown for particular geometry and flow condition.
Document ID
19740054788
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, S. S.
Johnson, M. L.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Subject Category
Aerodynamics
Meeting Information
Meeting: Meeting of the Acoustical Society of America
Location: New York, NY
Start Date: April 23, 1974
End Date: April 26, 1974
Sponsors: Acoustical Society of America
Accession Number
74A37538
Distribution Limits
Public
Copyright
Other

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