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Preliminary Comparison of Skin Friction Measurements with CFD PredictionsThe work to be described was performed at the NASA Langley UPWT (4-ft supersonic), test section #2, during 21-24 May 1996. The configuration being tested was the 1.675% Ref H controls model; test conditions were Ma = 2.40, Re = 3 million/ft. This was an exploration of a new technique, and it was not intended to provide definitive comparison of measured and computed skin friction results. It is, however, hoped that the experience gained will make such a rigorous comparison possible in the future.
Document ID
20000057265
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Kennelly, Robert A., Jr.
(NASA Ames Research Center Moffett Field, CA United States)
Lawrence, Scott L.
(NASA Ames Research Center Moffett Field, CA United States)
Flamm, Jeffrey D.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Publication Information
Publication: 1997 NASA High-Speed Research Program Aerodynamic Performance
Volume: 1
Issue: Part 2
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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