On parametric sensitivity of Reynolds-averaged Navier-Stokes SST turbulence model : 2D hypersonic shock-wave boundary-layer interactions /

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Bibliographic Details
Author / Creator:Brown, James L., author.
Imprint:Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, May 2014.
Description:1 online resource (61 pages) : color illustrations.
Series:NASA/TM ; 2014-218353
NASA technical memorandum ; 2014-218353.
Subject:Navier-Stokes equation.
Turbulence models.
Hypersonic shock.
Boundary layer separation.
Reynolds number.
Reynolds number.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10758080
Hidden Bibliographic Details
Varying Form of Title:2D hypersonic shock-wave boundary-layer interactions
Other authors / contributors:Ames Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Notes:Title from title screen (viewed Feb. 10, 2016).
"May 2014."
Includes bibliographical references (pages 35-39).
Sponsored by the National Aeronautics and Space Administration L-
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2014-218353

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