Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 /

Bibliographic Details

Main Authors:	Karabinus, Raymond J. (Author), Sanders, Bobby W. (Author)
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, May 1970.
Series:	NASA technical memorandum ; X-2009.
Subjects:	Mach number. Supersonic wind tunnels. Facilities.
Online Access:	https://purl.fdlp.gov/GPO/gpo189147