首页> 外文会议>International Symposium on Heat Transfer Enhancement and Energy Conservation >FILM COOLING PERFORMANCE AND HEAT TRANSFER OVER AN INCLINED FILM-COOLED SURFACE AT DIFFERENT DIVERGENT ANGLES WITH ESPECT TO THE HIGHLY TURBULENT MAINSTREAM
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FILM COOLING PERFORMANCE AND HEAT TRANSFER OVER AN INCLINED FILM-COOLED SURFACE AT DIFFERENT DIVERGENT ANGLES WITH ESPECT TO THE HIGHLY TURBULENT MAINSTREAM

机译:在不同的发散角度下膜冷却性能和传热在倾斜的薄膜冷却表面上,以备份到高度湍流的主流

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Experiments have been performed to study and obtain the adiabatic-wall film cooling effectiveness and the heat transfer over a film-cooled surface that is made inclined at various angles with respect to a highly turbulent flow. The vertical temperature distribution was measured to infer the flow structure and the rate of mixing of film jet with the freestream. The freestream turbulence intensity is controlled which ranges from 1.0% to 26.4%, the inclination or the divergent angle of the film-cooled surface ranges from 0° to 20°, the blowing parameter from 0.5 to 2.0. It is found that the mixing of the film jet with the freestream is significantly enhanced by both the freestream turbulence intensity and the divergent angle of the film-cooled surface, which leads to the decrease in the film cooling effectiveness and the increase in the heat transfer. However, the inclination angle has more effect on the film cooling performance while the turbulence intensity has more effect on the heat transfer under the film. More detailed discussion will be presented. Correlations for both the film cooling effectiveness and the heat transfer under the film-cooled surface have been very successful and will be provided.
机译:已经进行了实验以研究和获得绝热 - 壁膜冷却效果和在膜冷表面上的热传递,该膜冷却表面以各种角度倾斜于高度湍流。测量垂直温度分布以推断流动结构和薄膜射流与自由流动​​的混合速率。控制自由流湍流强度,其范围为1.0%至26.4%,薄膜冷却表面的倾斜度或发散角范围为0°至20°,吹入参数为0.5至2.0。发现薄膜射流与FreeStream的混合通过FreeStream湍流强度和薄膜冷却表面的发散角度显着提高,这导致薄膜冷却效果的降低和热传递的增加。然而,倾斜角对薄膜冷却性能产生更多影响,而湍流强度对薄膜下的热传递产生更多影响。将提出更详细的讨论。薄膜冷却效能和薄膜冷却表面下的热传递的相关性非常成功,并将提供。

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