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The application of cryogenics to high Reynolds number testing in wind tunnels. II - Development and application of the cryogenic wind tunnel conceptThe development and application of the cryogenic wind tunnel concept at the Langley Research Center are described. Particular attention is given to the low-speed cryogenic tunnel and the pilot transonic cryogenic tunnel. The major conclusions with respect to the operation and performance of the pilot transonic cryogenic tunnel after almost 4000 h of operation at cryogenic temperatures are that: (1) purging, cooldown, and warm-up times are acceptable and can be predicted with good accuracy, and that (2) the quantity of liquid nitrogen required for cooldown and running can be predicted with good accuracy. The U.S. National Transonic Facility is described in detail.
Document ID
19880066620
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kilgore, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Dress, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
September 1, 1984
Publication Information
Publication: Cryogenics
ISSN: 0011-2275
Subject Category
Research And Support Facilities (Air)
Accession Number
88A53847
Distribution Limits
Public
Copyright
Other

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