General purpose versus special algorithms for high-speed flows with shocks

In this paper we compare the performance of a new general algorithm developed recently in application to problems of high Mach number flows with the performance of specialised algorithms applicable only to such flows. It appears that the results for most examples compare well, the biggest difference...

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Published inInternational journal for numerical methods in fluids Vol. 27; no. 1-4; pp. 57 - 80
Main Authors Sai, B. V. K. Satya, Zienkiewicz, O. C., Manzari, M. T., Lyra, P. R. M., Morgan, K.
Format Journal Article
LanguageEnglish
Published Sussex John Wiley & Sons, Ltd 01.01.1998
Subjects
computational fluid dynamics
high speed flow
numerical method
shock modelling
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ISSN0271-2091
1097-0363
DOI10.1002/(SICI)1097-0363(199801)27:1/4<57::AID-FLD650>3.0.CO;2-C

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Summary:In this paper we compare the performance of a new general algorithm developed recently in application to problems of high Mach number flows with the performance of specialised algorithms applicable only to such flows. It appears that the results for most examples compare well, the biggest difference occurring in that of high Mach number compression corner. © 1998 John Wiley & Sons, Ltd.
Bibliography:ark:/67375/WNG-F3QH5D6Z-Q
NASA - No. NAGW/2127 (AMES 90-144)
istex:AD2C6DE0083E1853136A09B0F143451119B06429
ArticleID:FLD650
ObjectType-Article-2
SourceType-Scholarly Journals-1
ObjectType-Feature-1
content type line 23
ISSN:0271-2091
1097-0363
DOI:10.1002/(SICI)1097-0363(199801)27:1/4<57::AID-FLD650>3.0.CO;2-C