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Spectral methods for inviscid, compressible flowsReport developments in the application of spectral methods to two dimensional compressible flows are reviewed. A brief introduction to spectral methods -- their history and especially their implementation -- is provided. The stress is on those techniques relevant to transonic flow computation. The spectral multigrid iterative methods are discussed with application to the transonic full potential equation. Discontinuous solutions of the Euler equations are considered. The key element is the shock fitting technique which is briefly explained.
Document ID
19830025576
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hussaini, M. Y.
(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
July 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:172170
NASA-CR-172170
REPT-83-31
Report Number: NAS 1.26:172170
Report Number: NASA-CR-172170
Report Number: REPT-83-31
Accession Number
83N33847
Funding Number(s)
CONTRACT_GRANT: NAS1-17130
CONTRACT_GRANT: NAS1-16394
CONTRACT_GRANT: NAG1-109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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