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Adaptive remeshing for three-dimensional compressible flow computationsA practical solution algorithm for steady 3D Euler flows is presented. This algorithm employs coupling of a surface triangulator, an automatic tetrahedral mesh generator, an unstructured grid flow solver, and an error estimation procedure. The performance of the method is illustrated using a shock interaction problem in high Mach number flow over a swept circular cylinder.
Document ID
19930034854
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Peraire, J.
(NASA Langley Research Center Hampton, VA, United States)
Peiro, J.
(Imperial College of Science, Technology, and Medicine London, United Kingdom)
Morgan, K.
(Swansea Univ. College, United Kingdom)
Date Acquired
August 15, 2013
Publication Date
December 1, 1992
Publication Information
Publication: Journal of Computational Physics
Volume: 103
Issue: 2
ISSN: 0021-9991
Subject Category
Aerodynamics
Accession Number
93A18851
Funding Number(s)
CONTRACT_GRANT: NAGW-1809
CONTRACT_GRANT: NAGW-478
Distribution Limits
Public
Copyright
Other

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