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AeroacousticsAn analysis was conducted to determine the properties of sound generated by aerodynamic forces or motions originating in a flow, such as the unsteady aerodynamic forces on propellers or by turbulent flows around an aircraft. The acoustics of moving media are reviewed and mathematical models are developed. Lighthill's acoustic analogy and the application to turbulent flows are analyzed. The effects of solid boundaries are calculated. Theories based on the solution of linearized vorticity and acoustic field equations are explained. The effects of nonuniform mean flow on the generation of sound are reported.
Document ID
19740027005
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Authors
Goldstein, M., E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Physics, General
Report/Patent Number
NASA-SP-346
Accession Number
74N35118
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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