(Русский) Исследование инициирования недосжатой детонации стримерным и присоединенным СВЧ разрядом
(Русский) В настоящее время, на современных летательных аппаратах даже на сверхзвуковых скоростях потока воздух тормозится в воздухозаборнике до дозвуковых скоростей.
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(Русский) Base pressure oscillations and safety of load launching into orbit
(Русский) Physical details regarding base pressure low-frequency oscillations between rocket nozzles, their excitation and maintenance, are considered.
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(Русский) Detonation Jet Engine. Part II – Construction Features
(Русский) We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion.
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(Русский) Detonation Jet Engine. Part 1 – Thermodynamic Cycle
(Русский) We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion.
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