Secondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone /

Bibliographic Details

Main Author:	Li, Fei (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.
Series:	NASA technical memorandum ; 2015-218997.
Subjects:	Boundary layer flow. Circular cones. Cross flow. Hypersonic boundary layer. Vortices.
Online Access:	https://purl.fdlp.gov/GPO/gpo67293 http://purl.fdlp.gov/GPO/gpo67293