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Cryogenic wind tunnelsCryogenic wind tunnels and their use for high Reynolds number testing are reviewed. Emphasis is given to operational and aerodynamic testing experience in the NASA Langley 0.3-m Transonic Cryogenic Tunnel. Areas covered include development of test techniques and aerodynamic testing in cryogenic tunnels. The use of advanced testing techniques to increase the value of cryogenic tunnels is recommended. These include adaptive wall test sections, using solid but flexible top and bottom walls, and magnetic suspension and balance systems.
Document ID
19900054671
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kilgore, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1989
Subject Category
Research And Support Facilities (Air)
Accession Number
90A41726
Distribution Limits
Public
Copyright
Other

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