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Cryogenic wind-tunnel technologyThe cryogenic concept and the advantages it offers with respect to achieving full scale Reynolds number in a moderate size tunnel at reasonable levels of dynamic pressure are described. Aspects which must be considered during the development of a facility that uses gaseous nitrogen as the test gas are examined. These include the properties of nitrogen, particularly at high pressure; isentropic expansion and normal shock flows in nitrogen; real gas ratios; and the problem of condensation. Sources of information on cryogenic technology are cited.
Document ID
19770020198
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kilgore, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: High Reynolds Number Res.
Subject Category
Research And Support Facilities (Air)
Accession Number
77N27142
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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