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横向喷流引起的三维复杂干扰流场结构研究 被引量:4

Study of a 3D complex interference flow field structure induced by transverse jet
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摘要 研究了横向喷流引起流动分离的干扰流场特性,利用表面压力分布测量和纹影、油流等试验方法研究了此类流场的细节结构,给出了干扰流场的结构分析图。 The interference flow field characteristic of flow separation induced by transverse jet was investigated. The detail structure of this kind of flow field was studied by pressure measurement, schlieren photo and oil visualization, and the sketches of the interference flow field structure were drawn.
出处 《流体力学实验与测量》 EI CSCD 北大核心 2004年第3期59-63,共5页 Experiments and Measurements in Fluid Mechanics
关键词 横向喷流 流动分离 超声速 干扰流场 结构分析图 supersonic transverse jet flow field structure
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参考文献3

  • 1ZUKOSKI E E, SPAID F W.Secondary injection of gases into a supersonic fow [J].AIAA Journal,1964,2(10).
  • 2BRADFORD B, PRICE GREGORY S ELLIOTr, MADARA OGOT.Experimental optimization of transverse jet injector geometries for mixinchg into a supersonic flow [R].AIAA Paper 98-3019, 1998.
  • 3TOMIOKA S, JACOBSEN L S, SCHETZ J A.Interaction between a supersonic airstream and a sonic jet injected through a diamond-shaped orifice [ R], AIAA2000-0088,2000.

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