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.).
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.
Turbulence effects.
Turbulent flow.
Navier-Stokes equation.
Airplanes -- Scramjet engines.
Shock waves.
Turbulent boundary layer.
Format: E-Resource U.S. Federal Government Document Book
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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."
Includes bibliographical references (p. 14-16).
Sponsored by National Aeronautics and Space Administration WBS 031102.02.03.0829.11
GPO item no.:0830-D (online) classification:NAS 1.15:2012-217277