Detonation Jet Engine. Part 1 – Thermodynamic Cycle
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. The efficiency advantages of thermodynamic detonative combustion cycle over Humphrey combustion cycle at constant volume and Brayton combustion cycle at constant pressure were demonstrated. An ideal Ficket-Jacobs detonation cycle, and the thermodynamic cycle of real detonation engine that utilizes over compressed detonation were discussed. Main trends in development of detonation engines were described. Relevant for nearest time problems and directions of research were 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 II – Construction Features
We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion.
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