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Some aspects of adapting computational mesh to complex flow domains and structures with application to blown shock layer and base flowSeveral aspects connected with the notion of computation with flow oriented mesh systems are presented. Simple, effective approaches to the ideas discussed are demonstrated in current applications to blown forebody shock layer flow and full bluff body shock layer flow including the massively separated wake region.
Document ID
19810006202
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lombard, C. K. (PEDA Corp. Palo Alto, CA, United States)
Lombard, M. P. (PEDA Corp. Palo Alto, CA, United States)
Menees, G. P. (PEDA Corp. Palo Alto, CA, United States)
Yang, J. Y. (PEDA Corp. Palo Alto, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Publication Information
Publication: NASA. Langley Research Center Numerical Grid Generation Tech.
Subject Category
Numerical Analysis
Accession Number
81N14716
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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