Experimental investigation of hexcomb-pattern roughness effects on transition onset and turbulent heating augmentation at Mach 6 /

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, November 2019.
Series:	NASA technical memorandum ; 2019-220424.
Subjects:	Computational fluid dynamics. Hypersonic wind tunnels. Flow distribution. Aerothermodynamics. Correlation.
Online Access:	https://purl.fdlp.gov/GPO/gpo129673