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Real-Gas Aerothermodynamics Test FacilitiesThis chapter provides an overview of the current ground-based aerothermodynamic testing capabilities in Western Europe and the United States. The focus is on facilities capable of producing real-gas effects (dissociation, ionization, and thermochemical nonequilibrium) pertinent to the study of atmospheric flight in the Mach number range of 5 < M < 50. Perceived mission needs of interest to the Americans and Western Europeans are described where such real-gas flows are important.

The role of Computational Fluid Dynamics (CFD) in modern ground testing is discussed, and the capabilities of selected American and European real-gas facilities are described. An update on the current instrumentation in aerothermodynamic testing is also outlined.

Comments are made regarding the use of new facilities which have been brought on line during the past 3-5 years. Finally, future needs for aerothermodynamic testing, including instrumentation, are discussed and recommendations for implementation are reported.
Document ID
19990024923
Acquisition Source
Ames Research Center
Document Type
Contribution to a larger work
Authors
James 0. Arnold
(Ames Research Center Mountain View, California, United States)
George L. Seibert
(Wright Lab Wright-Patterson AFB, OH United States)
John F. Wendt.
(Von Karman Institute for Fluid Dynamics Sint-Genesius-Rode, Belgium)
Date Acquired
August 19, 2013
Publication Date
December 1, 1998
Publication Information
Publication: AGARD Advisory Report 319 - Hypersonic Experimental and Computational Capability, Improvement and Validation
Publisher: RTO/NATO /Canada Communication Group Inc.
Volume: 2
Issue Publication Date: December 1, 1998
ISBN: 92-836-1078-4
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Other
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