Cover Image

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
Description
Item Description:"November 2019."
Physical Description:1 online resource (vi, 143 pages, 1 unnumbered page) : color illustrations.
Bibliography:Includes bibliographical references (pages 10-11).