Interaction of shock waves with a jet wake during gas injection into supersonic stream

被引：0
|
作者：
V. N. Zudov
P. K. Tretyakov
机构：
[1] Khristianovich Institute of Theoretical and Applied Mechanics SB RAS,
来源：
Thermophysics and Aeromechanics | 2010年 / 17卷
关键词：
shock wave; subsonic jet; gas injection;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
In the present paper, we report the results of an experimental study of the interaction region of a planar compression shock produced by a wedge in stream with the wake formed behind a cocurrent gas jet (H2, air, or Ar) injected into the flow. Depending on the gas jet parameters, three modes of interaction could be distinguished: a strong interaction, observed when the flow velocity in the wake was subsonic; a moderate interaction, observed when a subsonic flow region, bounded by a shock of almost conical shape, formed in the vicinity of the compression shock; and a neutral interaction. Three-dimensional non-stationary Euler equations were solved to numerically examine the interaction of an axisymmetric jet with an oblique shock wave. The obtained interaction regimes were found to be in a reasonable agreement with experimental data.
引用
收藏
页码：543 / 549
页数：6
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