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

Bibliographic Details
Main Author: Davis, David O. (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
Series:NASA technical memorandum ; 2015-218841.
Subjects:
Boundary layers.
Computational fluid dynamics.
Shock wave interaction.
Flow measurement.
Turbulent flow.
Online Access:https://purl.fdlp.gov/GPO/gpo64648
http://purl.fdlp.gov/GPO/gpo64648
Description
Item Description: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
Physical Description:1 online resource (13 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 13).