Experimental database with baseline CFD solutions : 2-D and axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions /

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Bibliographic Details
Author / Creator:Marvin, Joseph G., author.
Imprint:Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, November 2013.
Description:1 online resource (123 pages) : illustrations.
Series:NASA/TM ; 2013-216604
NASA technical memorandum ; 2013-216604.
Subject:Hypersonic shock.
Turbulent boundary layer.
Computational fluid dynamics.
Two dimensional flow.
Navier-Stokes equation.
Hypersonic heat transfer.
Computational fluid dynamics.
Turbulent boundary layer.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10297462
Hidden Bibliographic Details
Varying Form of Title:Experimental database with baseline Computational Fluid Dynamics solutions
2-D and axisymmetric hypersonic shock wave turbulent boundary layer interactions
Other authors / contributors:Brown, James L., author.
Gnoffo, Peter A., author.
Ames Research Center, issuing body.
Notes:Title from title screen (viewed March 25, 2015).
"November 2013."
Includes bibliographical references.
Sponsored by the [NASA Ames Research Center] [NNA10DE12C] [WBS 470883.04.01.01]
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2013-216604

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