Review of Experimental work performed at the hypersonic aerodynamic shock tube

Авторы: Kotov M.A., Ruleva L.B., Solodovnikov S.I., Surzhikov S.T.
Сборник: International conference on the Methods of Aerophysical Research (ICMAR 2018) August 13 – 19, 2018, Novosibirsk, Russia, Abstracts
Серия: XIX ICMAR
Том: 1
Тезисы
Год издания: 2018
Место издания: Параллель Новосибирск Novosibirsk, Russia
Первая страница: 147
Последняя страница: 148
Аннотация: The input devices of air intake of a hypersonic ramjet engine with cavities simulating the combustion chamber in the form of a model group with sharp/blunt edges and different mutual orientation were investigated (different configurations of scramjet). Also particular attention was paid to shock-wave interaction over prospective space vehicles.
Добавил в систему: Рулева Лариса Борисовна

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