Large eddy simulation of transonic flow field in NASA rotor 37 /

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Bibliographic Details
Author / Creator:Hah, C.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2009]
Description:1 online resource (18 pages) : illustrations.
Language:English
Series:NASA TM- ; 2009-215627
NASA technical memorandum ; 2009-215627.
Subject:Transonic compressors.
Pressure distribution.
Large eddy simulation.
Navier-Stokes equation.
Computational fluid dynamics.
Flow characteristics.
Reynolds averaging.
Separated flow.
Turbulent flow.
Boundary layer separation.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8067300
Hidden Bibliographic Details
Other authors / contributors:NASA Glenn Research Center.
AIAA Aerospace Sciences Meeting (47th : 2009 : Orlando, Fla.)
Notes:Title from title screen (viewed on June 11, 2010).
"September 2009."
Includes bibliographical references (pages 6-7).
National Aeronautics and Space Administration WBS 561581.02.08.03.21.02.
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2009-215627