Volume 33 Issue 04
Apr.  2007
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Ding Shuiting, Hou Xiaojing, Xu Guoqiang, et al. Film bleeding on internal cooling in rectangular channel[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(04): 418-421. (in Chinese)
Citation: Ding Shuiting, Hou Xiaojing, Xu Guoqiang, et al. Film bleeding on internal cooling in rectangular channel[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(04): 418-421. (in Chinese)

Film bleeding on internal cooling in rectangular channel

  • Received Date: 09 May 2006
  • Publish Date: 30 Apr 2007
  • An experimental study was made to obtain heat transfer data in a rectangular channel with two ribs and nine holes. The objectives were to investigate the effect of mass flow ratios and bleed holes area ratio on internal cooling. Test was performed with single bleed hole as well as with multiple holes. Steady-state heat transfer coefficients were obtained using thermochromic liquid crystal. The heat transfer enhancement was observed to largely depend on the placement of bleed hole on the inter-ribs surface. It was found that the area-averaged Nusselt number was enhanced more by placing the bleed hole behind the rib. The best enhancement occurred between 6% and 8%. The heat transfer of effective was improved obviously when the Renolds number was low relatively. Some conclusion can be obtained that the heat transfer was enhanced at the regions from the edge of holes to downstream section. The influence of area flow ratio was also tested. It was found that the best area flow ratio was about 2.5%~3.0%.

     

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  • [1] 刘湘云. 有气膜孔和扰流肋的变截面回转通道内流阻与换热特性研究. 北京:北京航空航天大学能源与动力工程 学院,2005 Liu Xiangyun. The experimental research of pressure drop and heat transfer in sectional-cross U-shape duct. Beijing:School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, 2005 (in Chinese) [2] Thurman D, Poinsatte P. Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed[J]. ASME J Turbomachinery, 2001,123:90-96 [3] Byerlry A R, Jones T V, Ireland P T. Internal cooling passage heat transfer near the entrance to a film cooling hole:experimental and computational results. ASME 92-GT-241,1992 [4] Shen J R, Ireland P T. Heat transfer coefficient enhancement in a gas turbine blade cooling passage due to film cooling holes. IMECHE C434/040,1991 [5] Li Li, Ding S T, Xu G Q, et al. Experimental study on heat transfer in the compound cooling passage. ASME GT2006-90250,2006
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