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A Simplified Method for Estimating the Performance of Supersonic Ram-Jets
Published online by Cambridge University Press: 07 June 2016
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.
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- Research Article
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- Copyright © Royal Aeronautical Society. 1958
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