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The cryogenic transonic wind tunnel for high Reynolds number researchBased on theoretical studies and experience with a low speed cryogenic tunnel and with the transonic cryogenic tunnel, the cryogenic wind tunnel concept has been shown to offer many advantages with respect to the attainment of full scale Reynolds number at reasonable levels of dynamic pressure in a ground based facility. The unique modes of operation available in a pressurized cryogenic tunnel make possible for the first time the separation of Mach number, Reynolds number, and aeroelastic effects.
Document ID
19760018126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kilgore, R. A. (NASA Langley Research Center Hampton, VA, United States)
Adcock, J. B. (NASA Langley Research Center Hampton, VA, United States)
Ray, E. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: AGARD Wind Tunnel Design and Testing Tech.
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
L-10032
Accession Number
76N25214
Distribution Limits
Public
Copyright
Other
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