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Calculations Of Transonic Flow About A WingReport describes calculations of transonic airflows about wing in wind tunnel. Basic equations of flow used in study are Reynolds-averaged Navier-Stokes equations in strong conservation-law form. Equations of flow incorporated into finite-difference computer code called TNS (Transonic Navier-Stokes). Computational grid generated by solution of partial differential equations yielding smooth meshes conforming to surfaces of wing and wind tunnel.
Document ID
19880000253
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Holst, Terry L. (NASA Ames Research Center, Moffett Field, Calif.)
Gundy, Karen L. (NASA Ames Research Center, Moffett Field, Calif.)
Flores, Jolen (NASA Ames Research Center, Moffett Field, Calif.)
Chaderjian, Neal (NASA Ames Research Center, Moffett Field, Calif.)
Kaynak, Univer (Stanford University)
Thomas, Scott D. (Sterling Software)
Date Acquired
August 13, 2013
Publication Date
April 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11803
Accession Number
88B10253
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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