Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 /

Bibliographic Details

Main Author:	Hollis, Brian R. (Brian Ray) (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2017.
Series:	NASA technical memorandum ; 2017-219613.
Subjects:	Boundary layer transition. Hypersonic wind tunnels. Surface roughness. Surface roughness effects. Thermography.
Online Access:	https://purl.fdlp.gov/GPO/gpo82540 http://purl.fdlp.gov/GPO/gpo82540