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.
Physical details regarding base pressure low-frequency oscillations between rocket nozzles, their excitation and maintenance, are considered. Amplitude – frequency characteristics of these oscillations, as well as sequence of their type change, are studied. A single nozzle, a two-nozzle unit and a ring nozzle imitating multi-nozzle unit, are investigated in the present study.
Base pressure oscillations and safety of load launching into orbit
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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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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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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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