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

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 / George T. Carson, Jr., and Milton Lamb.

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Bibliographic Details
Online Access: Online Access
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:
Jet nozzles > Testing.
Nozzle geometry.
Mach number.
Hypersonic nozzles.
Ramjet engines.
Nozzle efficiency.

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Call Number: NAS 1.60:2814
NAS 1.60:2814 Available

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