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Model experience in the Langley 0.3-m transonic cryogenic tunnelThe model building, development, and testing experience gained during 8 years of operation of the 0.3-m Transonic Cryogenic Tunnel (TCT) is summarized. The summary is divided into four portions: (1) models tested in the 0.3-m TCT's original octagonal test section; (2) models tested in the present two dimensional test section; (3) models tested as a part of tunnel calibration and the development of advanced technology airfoils; and (4) development of a new way to construct two dimensional airfoil models. Design requirements imposed on the models by high Reynolds number testing at cryogenic temperatures are reviewed.
Document ID
19810022594
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lawing, P. L.
(NASA Langley Research Center Hampton, VA, United States)
Kilgore, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Publication Information
Publication: High Reynolds Number Res. - 1980
Subject Category
Aerodynamics
Accession Number
81N31136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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