Problems associated with operation at hypersonic speeds can be alleviated by operating engine combustion chamber at supersonic mean inlet velocities; governing equations for engine performance with normal detonation wave in chamber are derived; flight regime for which combustion through normal detonation is possible is investigated; performance of ideal detonative ramjet using acetylene fuel is presented for flight Mach numbers of 6 to 10; ramjet engine configuration for performance with normal detonation.
Hypersonic ramjet using normal detonation wave
Research Council Israel -- Bul
Israel Research Council -- Bulletin ; 8C , n 1
1960
12 pages
Report
English
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Detonation wave hypersonic ramjet
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