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Experimental and Numerical Study of Wall Flow Pattern of Turbine Cascade with Tip Clearance
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作者 杨庆海 黄洪雁 +1 位作者 韩万今 王仲奇 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2001年第4期210-216,共7页
By means of flow visualization on the wall surface and three dimensional flow field numerical simulation for the turbine cascade with 3.6% relative tip clearance, characteristics of the wall flow of the turbine cascad... By means of flow visualization on the wall surface and three dimensional flow field numerical simulation for the turbine cascade with 3.6% relative tip clearance, characteristics of the wall flow of the turbine cascade with large tip clearance is analyzed. The flow pattern on the wall surface near the trailing edge is especially discussed in detail by numerical simulation. Results of the experimental and numerical simulation show that the flow near the cascade trailing edge is very complex, and the wall flow patterns near the upper and down trailing edges are clearly different due to the influence of blade tip clearance. 展开更多
关键词 axial flow turbomachinery Cascades (fluid mechanics) Computer simulation Flow patterns Flow visualization Wall flow
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