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Reacting flowsFeatures of chemically reacting separated hypersonic flows are identified and issues concerning their analysis and simulation are discussed. Emphasis is placed on flows of high temperature dissociating and ionizing air and current methods for studying and characterizing these flows, including separation, are reviewed. The aeroassist orbital transfer vehicle and its flight trajectory are used for illustration. Thermochemical nonequilibrium phenomena are emphasized and extension of continuum analysis to the high altitude slip-flow regime is considered.
Document ID
19900008257
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Deiwert, George S.
(NASA Ames Research Center Moffett Field, CA, United States)
Candler, Graham V.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Publication Information
Publication: AGARD, Special Course on Three-Dimensional Supersonic(Hypersonic Flows Including Separation
Subject Category
Aerodynamics
Accession Number
90N17573
Distribution Limits
Public
Copyright
Other
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