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Film-Cooling Performance and Heat Transfer over an Inclined Film-Cooled Surface

机译:倾斜的薄膜冷却表面上的薄膜冷却性能和传热

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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 uniform flow. The vertical temperature distribution was measured to infer the flow structure and the rate of mixing of the film jet with the freestream. The inclination angle of the film-cooled surface ranges from -20 to 20 deg with an increment of 5 deg, the blowing parameter from 0.5 to 2.0 (0.5,0.7,1.0,1.5,2.0). It is found that the mixing of the film jet with the freestream is significantly affected by the inclination angle of the film-cooled surface. The divergence of the film-cooled surface can make the flow unstable and cause flow separation, whereas the convergence has both stabilization and impingement effects on the film jet. This has a very complicated effect on both the film-cooling performance and the heat transfer under the film. More detailed discussion on the flow and the heat transfer is presented. Correlations for both the film-cooling effectiveness and the heat transfer under the film are provided.
机译:已经进行了实验以研究并获得绝热壁的膜冷却效果以及在相对于均匀流动倾斜各种角度的膜冷却表面上的热传递。测量垂直温度分布以推断薄膜射流与自由流的流动结构和混合速率。薄膜冷却表面的倾斜角度范围为-20至20度,以5度为增量,吹塑参数为0.5至2.0(0.5,0.7,1.0,1.5,2.0)。已经发现,薄膜射流与自由流的混合受到薄膜冷却表面的倾斜角的显着影响。薄膜冷却表面的发散会导致流动不稳定并引起流动分离,而会聚对薄膜射流既有稳定作用又有撞击作用。这对薄膜的冷却性能和薄膜下的热传递都有非常复杂的影响。提出了关于流动和传热的更详细的讨论。提供了膜冷却效率和膜下的热传递的相关性。

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