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Calculating Shocks In Flows At Chemical EquilibriumBoundary conditions prove critical. Conference paper describes algorithm for calculation of shocks in hypersonic flows of gases at chemical equilibrium. Although algorithm represents intermediate stage in development of reliable, accurate computer code for two-dimensional flow, research leading up to it contributes to understanding of what is needed to complete task.
Document ID
19880000480
Document Type
Other - NASA Tech Brief
Authors
Eberhardt, Scott (NASA Ames Research Center, Moffett Field, Calif.)
Palmer, Grant (NASA Ames Research Center, Moffett Field, Calif.)
Date Acquired
August 13, 2013
Publication Date
October 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 9
ISSN: 0145-319X
Subject Category
PHYSICAL SCIENCES
Report/Patent Number
ARC-11741
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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