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

Bibliographic Details

Main Author:	Castner, Raymond S.
Corporate Authors:	NASA Glenn Research Center, AIAA Applied Aerodynamics Conference
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Series:	NASA technical memorandum ; 217137.
Subjects:	Exhaust nozzles. Nozzle flow. Plumes. Supersonic aircraft. Computational fluid dynamics. Nozzle geometry. Pressure ratio. Shock waves. Elastic waves.
Online Access:	https://purl.fdlp.gov/GPO/gpo27499