High-enthalpy hot-shot wind tunnel with combined heating and stabilization of parameters

Маслов, А. А.; Shumsky, V. V.; Yaroslavtsev, M. I.

doi:10.1134/s0869864313050011

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Cited by 16 publications

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“…1). Форкамера аэродинамической трубы IT-302M использовалась в качестве источника высокоэнтальпийного газа [9]. Эксперименты проводились в режиме присоединительного трубопровода.…”

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Взаимодействие Газовых Струй Со Сверхзвуковым Поперечным Потоком В Канале

Голубев¹,

Гольдфельд²

2019

Письма В Журнал Технической Физики

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The results of a study on the hydrogen sound jets penetrating a cross flow at Mach 4 and their influence on the flow structure in a backward facing step (BFS) channel are presented. It is shown that jet penetration in a channel differs from penetration in a free stream and cannot be predicted using the well-known empirical relations. Due to the influence of the reflected shock wave and its interaction with the wall boundary layer, an increase in the hydrogen jet-to-crossflow momentum flux ratio leads to a change in the flow structure and pressure distribution in the jet injection area and downstream after the backward facing BFS.

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