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NASA NTRS ยท 19770020198

Cryogenic wind-tunnel technology

Abstract

The 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.

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BibTeXRIS

Kilgore, R. A.. 1977-01-01. Cryogenic wind-tunnel technology. https://ntrs.nasa.gov/citations/19770020198

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