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Review of the advanced technology airfoil test program in the 0.3-meter transonic cryogenic tunnelThe following areas were addressed: interchangeable test sections in the 0.3-M Transonic Cryogenic Tunnel (TCT); typical airfoil installation; airfoil capability; advanced technology airfoil test (ATAT); effects of the Reynolds number on the normal force coefficient; effects of the Reynolds number on the drag coefficient; and comparison of experimental results with theory.
Document ID
19850003725
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ray, E. J. (NASA Langley Research Center Hampton, VA, United States)
Ladson, C. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: Wind Tunnel Wall Interference Assessment and Correction, 1983
Subject Category
Aerodynamics
Accession Number
85N12033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19850003703Collected WorksWind Tunnel Wall Interference Assessment and Correction, 1983
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