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Langley's two-dimensional research facilities: Capabilities and plansThe current capabilities and the forthcoming plans for Langley's two-dimensional research facilities are described. The characteristics of the Langley facilities are discussed in terms of Reynolds number, Mach number, and angle-of-attack capabilities. Comments are made with regard to the approaches which have been investigated to alleviate typical problem areas such as wall boundary effects. Because of the need for increased Reynolds number capability at high subsonic speeds, a considerable portion of the paper deals with a description of the 20 by 60 cm two-dimensional test section of the Langley 0.3 meter transonic cryogenic tunnel which is currently in the calibration and shakedown phase.
Document ID
19790011884
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ray, E. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Advanced Technol. Airfoil Res., Vol. 1, Pt. 1
Subject Category
Aerodynamics
Accession Number
79N20055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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