On the possible formation of a vortex flow in a supersonic inlet with three-dimensional compression

被引：0
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作者：
A. V. Lokotko
A. M. Kharitonov
机构：
来源：
Fluid Dynamics | 2006年 / 41卷
关键词：
air-intake; rocket-ramjet engine; jet injection; air duct; vortex flow; vortex breakdown;
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学科分类号：
摘要：
The structure of the flow in an inlet with three-dimensional compression and an adjoining channel of rectangular cross-section is experimentally investigated for the external flow parameters M∞ = 4 and Re ≈ 52 · 106 1/m. The phenomenon of vortex generation in the air-intake and its breakdown at the channel entry, where it encounters an elevated pressure gradient, is studied
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页码：649 / 660
页数：11
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