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:	Turbulent boundary layer. Hypersonic flight. Large eddy simulation. Supersonic combustion ramjet engines. Reynolds averaging. SHOCK WAVES. Turbulence effects. Turbulent flow. Navier-Stokes equation. Airplanes -- Scramjet engines. Shock waves. Turbulence. Turbulent boundary layer.
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

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