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首页> 外文期刊>Journal of Thermal Science and Engineering Applications: Transactions of the ASME >Enhancement of Film Cooling Effectiveness Using Rectangular Winglet Pair
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Enhancement of Film Cooling Effectiveness Using Rectangular Winglet Pair

机译:使用矩形小翼对增强薄膜冷却效果

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This study deals with the film cooling enhancement in a combustion chamber by the use of rectangular winglet vortex generators (VGs). Rectangular winglet pair (RWP) in both the common-flow up and the common-flow down configuration is installed upstream of a coolant injection hole on the lower chamber wall. A three-dimensional numerical approach with complete solution of Navier-Stokes (NS) equations closed by the k-epsilon turbulence model is used for analyzing the effect of VG installation on film cooling effectiveness enhancement. The effect of RWP orientation is investigated to deduce the best configuration which is then optimized in terms of its geometrical parameters including its upstream distance from the hole and the angle it makes with the incoming flow. Results obtained show that a RWP located upstream of the coolant hole in common-flow down configuration gives the best effectiveness enhancement with certain other geometrical parameters specified. A novel "mushroom" adiabatic distribution scheme for film cooling effectiveness and temperature has been discussed in the paper. This characteristic scheme is developed as a result of RWPs' vortices interaction with the coolant inlet jet and the hot mainstream flow. A detailed discussion of the mechanisms and the flow field properties underlying the effectiveness enhancement and other phenomenon observed has also been presented in the paper.
机译:本文研究了矩形小翼涡发生器(VG)对燃烧室气膜冷却的强化作用。在下腔室壁上的冷却剂注入孔的上游,安装有共同向上流动和共同向下流动配置的矩形小翼对(RWP)。采用三维数值方法,通过完全求解由k-epsilon湍流模型封闭的Navier-Stokes(NS)方程,分析了VG装置对气膜冷却效率提高的影响。研究RWP方向的影响,以推断最佳配置,然后根据其几何参数(包括其与孔的上游距离以及其与流入流的夹角)进行优化。结果表明,在通常的降流结构中,位于冷却剂孔上游的RWP在指定其他某些几何参数的情况下提供了最佳的效率增强。本文讨论了一种新的气膜冷却效率和温度的“蘑菇”绝热分布方案。这种特征方案是RWP涡与冷却剂入口射流和热主流流相互作用的结果。文中还详细讨论了有效性增强和观察到的其他现象的机理和流场特性。

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