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Supersonic Ramjet Performance

Supersonic Ramjet Performance Ideal and practical performance of ramjet units in steady flight in the stratosphere at Mach numbers from 15 to 4 is examined. The effects of combustion, temperature, altitude, intake and exhaust nozzle design are considered. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032342
Publisher site
See Article on Publisher Site

Abstract

Ideal and practical performance of ramjet units in steady flight in the stratosphere at Mach numbers from 15 to 4 is examined. The effects of combustion, temperature, altitude, intake and exhaust nozzle design are considered.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Oct 1, 1953

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