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A Simplified Method for Estimating the Performance of Supersonic Ram-Jets

Published online by Cambridge University Press:  07 June 2016

A. B. P. Beeton*
Affiliation:
National Gas Turbine Establishment
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Summary

Curves are presented which, together with a knowledge of the intake performance, enable ram-jet thrust coefficients and specific consumption figures to be obtained quickly and accurately in the range M = 1·0 to 3·0.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1958

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