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Predictions for the Effects of Free Stream Turbulence on Turbine Blade Heat Transfer

机译:自由流湍流对涡轮叶片传热影响的预测

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摘要

An approach to predicting the effects of free stream turbulence on turbine vane and blade heat transfer is described. Four models for predicting the effects of free stream turbulence were in incorporated into a Navier-Stokes CFD analysis. Predictions were compared with experimental data in order to identify an appropriate model for use across a wide range of flow conditions. The analyses were compared with data from five vane geometries and from four rotor geometries. Each of these nine geometries had data for different Reynolds numbers. Comparisons were made for twenty four cases. Steady state calculations were done because all experimental data were obtained in steady state tests. High turbulence levels often result in suction surface transition upstream of the throat, while at low to moderate Reynolds numbers the pressure surface remains laminar. A two-dimensional analysis was used because the flow is predominately two-dimensional in the regions where free stream turbulence significantly augments surface heat transfer. Because the evaluation of models for predicting turbulence effects can be affected by other factors, the paper discusses modeling for transition, relaminarization, and near wall damping. Quantitative comparisons are given between the predictions and data.
机译:描述了一种预测自由流湍流对涡轮机叶片和叶片传热的影响的方法。 Navier-Stokes CFD分析中纳入了四个用于预测自由流湍流影响的模型。将预测结果与实验数据进行比较,以确定适合在各种流动条件下使用的合适模型。将分析与来自五个叶片几何形状和来自四个转子几何形状的数据进行比较。这9个几何图形中的每一个都有不同雷诺数的数据。比较了二十四个案例。进行稳态计算是因为所有实验数据都是在稳态测试中获得的。高湍流度通常会导致喉咙上游的吸力面过渡,而在低至中等的雷诺数时,压力面仍保持层状。使用二维分析是因为在自由流湍流显着增加表面热传递的区域中,流动主要是二维的。由于用于预测湍流效应的模型的评估可能会受到其他因素的影响,因此本文讨论了过渡,再层化和近壁阻尼的建模。给出了预测和数据之间的定量比较。

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