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Rarefied FlowRarefaction effects are important for hypersonic applications for a wide spectrum of conditions ranging from low-density (high altitude) situations to relatively high-density flows where the characteristic dimension is small. The present chapter concentrates on two hypersonic flow problems at flow conditions that produce a significant range of rarefaction effects: corner flow with jet interaction and blunt body flow with special emphasis on the near wake, These problems were chosen because they involve complex flow interactions that have significant implications for both spacecraft and re-entry vehicles. In an effort to clarify issues associated with these two general flow problems and to enhance their respective databases, both experimental and computational contributions were executed by an international group of researchers. In some cases, multiple data sources for both experimental and computational contributions are achieved.
Document ID
19990024920
Acquisition Source
Langley Research Center
Document Type
Contribution to a larger work
Authors
James N. Moss
(Langley Research Center Hampton, Virginia, United States)
Jean-Claude Lengrand
(French National Centre for Scientific Research Paris, France)
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
Fluid Mechanics And Heat Transfer
Distribution Limits
Public
Copyright
Other
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