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Algorithm Computes Hypersonic Flow Of AirAlgorithm simulates three-dimensional hypersonic flow of air or another mixture of gases around blunt body. Accounts for nonequilibrium thermochemical effects via two-temperature mathematical model of molecular excitations and equations for finite-rate chemical reactions. These equations fully coupled to fluid dynamical equations.
Document ID
19910000444
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Palmer, Grant (NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
September 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 9
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
ARC-12623
Report Number: ARC-12623
ISSN: 0145-319X
Accession Number
91B10444
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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