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Vortices within the Separation Region in a Decelerating Channel Flow (Effect of Inlet Velocity Gradient)

Vortices within the Separation Region in a Decelerating Channel Flow (Effect of Inlet Velocity Gradient)
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摘要 An experimental investigation was made into three-dimensional separated flow and the vortices within the flow separation in a decelerating channel flow generated by the suction from a porous side wall. The flows along the side and bottom walls were visualized by the surface tuft method. The turbulent internal flow was measured by the split-film probe to investigate the turbulent flow including the reverse flow. In the flow visualization for the strong decelerating flow (the suction flow ratio:0.8), two typical flow patterns appear alternatively. One is that the flow near the bottom wall separates more upstream than the flow near the top wall and a clockwise vortex can be seen in the separation region. Another is the reversal flow pattern with a counterclockwise vortex. By the turbulent flow measurement using the split-film probe, two peaks of turbulence level are observed for the strong decelerating flow case. These peaks can be related with two flow patterns mentioned above.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2005年第4期341-345,共5页 热科学学报(英文版)
关键词 vortices within the separation decelerating channel flow turbulent flow split-film probe 旋涡 分离区域 减速通道 湍流
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参考文献3

  • 1Goto,A.Flow Visualization in a Low Specific Speed Diffuser Pump Stage (in Japanese)[].Turbomachinery.1995
  • 2Hah,C,Loellbach,J.Development of Hub Corner Stall and Its Influence on the Performance of Axial Compressor Blade Rows[].Journal of Turbomachinery.1999
  • 3Sasaki,K,Kiya,M.Turbulent Flow Measurement of the Reverse Flow by the Split Film Probe.Trans. Jpn. Soc. Mech. Eng[].Sen B.1985

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