Paper derives equations governing performance of ramjet using detonative combustion, and evaluates performance; engine layout permits normal detonation wave stabilized in diverging combustion chamber passage, or oblique wave stabilized on wedge; lower speed limit of detonative ramjet and cycle calculation; difficulties encountered by ramjets designed for hypersonic speeds may be alleviated if ramjet is designed to burn incoming air at supersonic velocities in stabilized detonation wave. (See also SAE -- Paper 419A for meeting Oct 9-13 1961 8 p)
Performance of hypersonic ramjet using detonative combustion
SAE -- J
Society of Automotive Engineers -- Journal ; 69 , n 11
1961
2 pages
Article (Journal)
English
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Performance of hypersonic Ramjet using detonative combustion
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