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Numerical investigation of flow and heat transfer in rotating trapezoidal channel with lateral slots and dimple structure

机译:横轴旋转梯形通道流动和传热的数值研究

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摘要

High-efficiency trailing edge cooling technology is essential for the safe and stable operation of turbine blades. In this paper, trapezoidal trailing edge channels with lateral slots are modeled, and a variety of dimples with different sizes and arrangement densities are placed on the end walls. Flow characteristics, wall heat transfer distributions and overall heat transfer performance under stationary and rotating states are numerically investigated and effects of dimple arrangement, rotation number (Ro) and channel orientation (β) are comprehensively analyzed. The results show that, under rotating state, the Coriolis force leads to the flow separation, while dimples promote the generation and development of three-dimensional spatial vortices, and effectively suppresses the expansion of separation area. Dimples greatly improve the rotating cooling performance, and there exists a critical point of arrangement density, in which the maximum heat transfer level is obtained. A 108.2% improvement in relative Nusselt number of trailing surface can be achieved by increasing rotation number in dimple channels. And the operation condition of Ro = 0.8 and β = 15° is recommended for the cooling of trapezoidal trailing edge. Compared with rotation number, the channel orientation has a stronger effect on the flow and heat transfer performances.
机译:高效后缘冷却技术对于涡轮叶片的安全和稳定运行至关重要。在本文中,建模具有横向槽的梯形后缘通道,并将各种具有不同尺寸和布置密度的凹坑放置在端壁上。在静止和旋转状态下的流动特性,壁传热分布和整体传热性能在数值上进行了数量研究,并综合地分析了浊度排列,旋转数(RO)和沟道取向(β)的影响。结果表明,在旋转状态下,科里奥利力导致流动分离,而凹槽促进了三维空间涡旋的产生和开发,并有效地抑制了分离区域的膨胀。凹坑大大提高了旋转冷却性能,存在临界排列密度,其中获得最大传热水平。通过增加凹坑通道中的旋转数来实现相对露珠尾部的相对露珠数的108.2%。并且建议为梯形后缘的冷却= 0.8和β= 15°的操作条件。与旋转数相比,通道取向对流动和传热性能具有更强的影响。

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