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Real Gas/Blunt ConeIn this chapter recent activity in real-gas database definition and code validation will be summarized. In the Phase I report of the Working Group (WG) 181, aerothermodynamic problems were classified, for purpose of discussion, into seven types: aerodynamic parameters, viscous/shock interaction, boundary-layer transition, forebody-heating/heat-transfer, radiation and ablation, lee and base-region flow, and low-density flow. Several of these problem types were the subject of various chapters of the Phase 1 report describing real-gas effects and ground test facility issues. In this chapter some background and objectives outlined in the real-Gas effects Chapter V of the Phase 1 report will be reviewed. The results of the blunt cone test campaign developed under the auspices of the WG18 activity to study real-gas phenomena will be summarized, including the experimental and computational programs, issues and questions, and recommendations. Further, recent progress in other real-gas areas beyond the blunt cone test campaign will be discussed. Finally, a summary in which the present status of our understanding of real-gas issues will be presented.
Document ID
19990024921
Acquisition Source
Ames Research Center
Document Type
Contribution to a larger work
Authors
George S. Delwert
(Ames Research Center Mountain View, California, United States)
Georg Eltetberg
(German Aerospace Center Cologne, Germany)
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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