CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction /

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Bibliographic Details
Author / Creator:Davis, David O., author.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
Description:1 online resource (13 pages) : color illustrations.
Series:NASA/TM ; 2015-218841
NASA technical memorandum ; 2015-218841.
Subject:Boundary layers.
Computational fluid dynamics.
Shock wave interaction.
Flow measurement.
Turbulent flow.
Computational fluid dynamics.
Flow meters.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:
Hidden Bibliographic Details
Varying Form of Title:Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction
Other authors / contributors:NASA Glenn Research Center, issuing body.
Notes:Title from title screen (viewed on Feb. 2, 2016).
"September 2015."
"Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015.
Includes bibliographical references (page 13).
GPO item no.:0830-D (online) classification:NAS 1.15:2015-218841