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Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /

Bibliographic Details
Main Authors:	Carson, George T. (Author), Lamb, Milton (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, June 1988.
Series:	NASA technical paper ; 2814.
Subjects:	Nozzle geometry. Mach number. Hypersonic nozzles. Ramjet engines. Nozzle efficiency. Jet nozzles > Testing.
Online Access:	https://purl.fdlp.gov/GPO/gpo106418

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