Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel /

Bibliographic Details

Main Author:	Durston, D. A. (Author)
Format:	Government Document eBook
Language:	English
Published:	Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, December 2018.
Series:	NASA technical publication ; 2018-219879.
Subjects:	Supersonic speed. Computational fluid dynamics. Supersonic wind tunnels. Mach number. Plumes.
Online Access:	https://purl.fdlp.gov/GPO/gpo121493