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Computational aeroacoustics using hyperbolic wave primitivesA compact high order three-spatial point, two-time level dissipationless scheme is derived by matching amplification factors from differential and difference forms hyperbolic systems of partial differential equations. This approach has the advantage of allowing large time steps (Courant numbers of one) and imposing boundary conditions that are globally compatible with the wave operators. Solutions are presented for planar and spherical one dimensional acoustic waves and more complex wave patterns in two dimensions.
Document ID
19950023715
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, Sanford S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: NASA. Langley Research Center,Hampton, VA. ICASE(LaRC Workshop on Benchmark Problems in Computational Aeroacoustics (CAA) p 27-45 (SEE N95-30133 10-71)
Subject Category
Acoustics
Accession Number
95N30136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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