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