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Spectral methods for the Euler equations: Chebyshev methods and shock-fittingThe Chebyshev spectral collocation method for the Euler gas-dynamic equations is described. It is used with shock fitting to compute several two-dimensional, gas-dynamic flows. Examples include a shock-acoustic wave interaction, a shock/vortex interaction, and the classical blunt body problem. With shock fitting, the spectral method has a clear advantage over second order finite differences in that equivalent accuracy can be obtained with far fewer grid points.
Document ID
19840009050
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hussaini, M. Y.
(NASA Langley Research Center Hampton, VA, United States)
Kopriva, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Salas, M. D.
(NASA Langley Research Center Hampton, VA, United States)
Zang, T. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.26:172295
NASA-CR-172295
Report Number: NAS 1.26:172295
Report Number: NASA-CR-172295
Accession Number
84N17118
Funding Number(s)
CONTRACT_GRANT: NAS1-17070
CONTRACT_GRANT: NAS1-17130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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