Status of turbulence modeling for hypersonic propulsion flowpaths /

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Bibliographic Details
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Description:1 online resource (28 p.) : ill. (some col.).
Language:English
Series:NASA/TM ; 2012-217277
NASA technical memorandum ; 2012-217277.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8930072
Hidden Bibliographic Details
Other authors / contributors:Georgiadis, Nicholas J.
NASA Glenn Research Center.
Joint Propulsion Conference and Exhibit (47 : 2011 : San Diego, Calif.)
Notes:Title from title screen (viewed on Oct. 2, 2012).
"April 2012."
"Prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE San Diego, California, July 31-August 3, 2011."
"AIAA-2011-5917."
Includes bibliographical references (p. 14-16).
Sponsored by National Aeronautics and Space Administration WBS 031102.02.03.0829.11
E-18032
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2012-217277

MARC

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650 7 |a Turbulent boundary layer.  |2 nasat 
650 7 |a Hypersonic flight.  |2 nasat 
650 7 |a Large eddy simulation.  |2 nasat 
650 7 |a Supersonic combustion ramjet engines.  |2 nasat 
650 7 |a Reynolds averaging.  |2 nasat 
650 7 |a SHOCK WAVES.  |2 nasat 
650 7 |a Turbulence effects.  |2 nasat 
650 7 |a Turbulent flow.  |2 nasat 
650 7 |a Navier-Stokes equation.  |2 nasat 
650 7 |a Airplanes  |x Scramjet engines.  |2 fast  |0 http://id.worldcat.org/fast/fst00803456 
650 7 |a Shock waves.  |2 fast  |0 http://id.worldcat.org/fast/fst01116729 
650 7 |a Turbulence.  |2 fast  |0 http://id.worldcat.org/fast/fst01159210 
650 7 |a Turbulent boundary layer.  |2 fast  |0 http://id.worldcat.org/fast/fst01159225 
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