Detonation Jet Engine. Part II – Construction Features
We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion.
We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion. Detonation engines of various concepts, pulse detonation, rotational and engine with stationary detonation wave, are reviewed. Main trends in detonation engine development are discussed. The most important works that carried out theoretical, experimental and computational research and their parametrical optimization are described. Relevant for nearest time problems and directions of research are formulated.
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Исследование инициирования недосжатой детонации стримерным и присоединенным СВЧ разрядом
В настоящее время, на современных летательных аппаратах даже на сверхзвуковых скоростях потока воздух тормозится в воздухозаборнике до дозвуковых скоростей.
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Base pressure oscillations and safety of load launching into orbit
Physical details regarding base pressure low-frequency oscillations between rocket nozzles, their excitation and maintenance, are considered.
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Detonation Jet Engine. Part 1 – Thermodynamic Cycle
We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion.
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