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Numerical Simulation on the Effect of Turbulence Models on Impingement Cooling of Double Chamber Model

机译:湍流模型对双室模型冲击冷却影响的数值模拟

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Investigation of the effects of impingement cooling for the different turbulence models and study of the aerodynamic behavior of a simplified transition piece model (TP) are the two themes of this paper. A model (double chamber model) of a one-fourth cylinder is designed which could simulate the transition piece structure and performance. The relative strengths and drawbacks of renormalization group theoryk-ε(RNG), the realizablek-ε(RKE), thev2-f, the shear stress transportk-ω(SST), and large-eddy simulation (LES) models are used to solve the closure problem. The prediction of the inner wall temperature, cooling effectiveness, and velocity magnitude contours in various conditions are compared in five different turbulence models. Surprisingly, thev2-fand SST models can produce even better predictions of fluid properties in impinging jet flows. It is recommended as the best compromise between solution speed and accuracy.
机译:研究冲击冷却对不同湍流模型的影响以及研究简化过渡件模型(TP)的空气动力学特性是本文的两个主题。设计了一个四分之一气缸模型(双室模型),该模型可以模拟过渡件的结构和性能。使用重归一化群理论k-ε(RNG),可实现的k-ε(RKE),v2-f,剪切应力传递k-ω(SST)和大涡模拟(LES)模型的相对优缺点进行求解关闭问题。在五个不同的湍流模型中,比较了各种条件下内壁温度,冷却效率和速度幅值等值线的预测。出乎意料的是,v2-fand SST模型可以对撞击射流产生更好的流体特性预测。建议将其作为解决方案速度和准确性之间的最佳折衷方案。

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