Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction /

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Bibliographic Details
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Description:1 online resource (28 p.) : col. ill.
Language:English
Series:NASA/TM ; 2011-216832
NASA technical memorandum ; 216832.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8536081
Hidden Bibliographic Details
Other authors / contributors:DeBonis, James R.
NASA Glenn Research Center.
AIAA Applied Aerodynamics Conference (28th : 2010 : Chicago, Ill.)
Notes:Title from title screen (viewed on Oct. 25, 2011).
"March 2011."
"AIAA-2010-4823."
Includes bibliographical references (p. 27-28).
WBS 984754.02.07.03.13.02
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2011-216832

MARC

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650 7 |a Shock wave interaction.  |2 nasat 
650 7 |a Boundary layers.  |2 nasat 
650 7 |a Turbulence models.  |2 nasat 
650 7 |a Computational fluid dynamics.  |2 nasat 
650 7 |a Navier-Stokes equation.  |2 nasat 
650 7 |a Large eddy simulation.  |2 nasat 
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