Exhaust nozzle plume effects on sonic boom test results for vectored nozzles /

Bibliographic Details

Main Author:	Castner, Raymond S.
Corporate Authors:	NASA Glenn Research Center, Joint Propulsion Conference and Exhibit
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 217229.
Subjects:	Exhaust nozzles. Sonic booms. Computational fluid dynamics. Elastic waves. Plumes. F-15 aircraft. Supersonic aircraft. Pressure ratio.
Online Access:	https://purl.fdlp.gov/GPO/gpo28438