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Prospects for computing airfoil aerodynamics with Reynolds averaged Navier-Stokes codesThe Reynolds averaged Navier-Stokes equations are solved numerically for a variety of transonic airfoil configurations where viscous phenomena are important. Illustrative examples include flows past sensitive geometries, Reynolds number effects, and buffet phenomena.
Document ID
19790011867
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Deiwert, G. S. (NASA Ames Research Center Moffett Field, CA, United States)
Bailey, H. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Langley Res. Center Advanced Technol. Airfoil Res., Vol. 1, Pt. 1
Subject Category
Aerodynamics
Accession Number
79N20038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19790011859Collected WorksAdvanced Technology Airfoil Research, volume 1, part 1
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