Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [electronic resource] / Raymond Castner.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Castner, Raymond S.
Corporate Authors:	NASA Glenn Research Center, Joint Propulsion Conference and Exhibit
Format:	Government Document Electronic 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.

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Call Number:	NAS 1.15:2012-217229
NAS 1.15:2012-217229	Available