Slot nozzle effects for reduced sonic boom on a generic supersonic wing section /

Bibliographic Details

Main Author:	Castner, Raymond S.
Corporate Authors:	NASA Glenn Research Center, AIAA Aerospace Sciences Meeting
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216258.
Subjects:	Exhaust nozzles. Sonic booms. Wing slots. Aircraft control. Computational fluid dynamics. Exhaust gases. Supersonic speed. Mach number. High aspect ratio.
Online Access:	https://purl.fdlp.gov/GPO/LPS126590