Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel /

Bibliographic Details
Main Author:	Castner, Raymond S. (Author)
Corporate Author:	Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
Series:	NASA technical memorandum ; 217903.
Subjects:	Pressure distribution. Sonic booms. Spatial distribution. Supersonic wind tunnels. Wind pressure.
Online Access:	https://purl.fdlp.gov/GPO/gpo53006 http://purl.fdlp.gov/GPO/gpo53006 http://purl.fdlp.gov/GPO/gpo51768

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