Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses /

Bibliographic Details

Main Author:	Friedlander, David J. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2013.
Series:	NASA technical memorandum ; 218081.
Subjects:	Computational fluid dynamics. Shock wave interaction. Boundary layers. Flow distribution. Particle image velocimetry. Large eddy simulation.
Online Access:	https://purl.fdlp.gov/GPO/gpo53705 http://purl.fdlp.gov/GPO/gpo53705