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Computing Flow Transition On Parallel ProcessorsParallel algorithm developed on multiple-microprocessor computer. Program initiated to develop computer codes capable of directly simulating and mathematically modeling transition process at mach numbers ranging from subsonic to hypersonic. Parallel computers potentially offer reduction of processing time; processing time inversely proportional to number of available processors.
Document ID
19930000651
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bokhari, S. (National Research Council)
Erlebacher, G. (NASA Langley Research Center, Hampton, VA.)
Hussaini, M. Y. (Institute for Computer Applications in Science and Engineering)
Date Acquired
August 16, 2013
Publication Date
October 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 10
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-14303
Accession Number
93B10651
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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