首页> 外文会议>American Society of Mechanical Engineers(ASME) Turbo Expo vol.3; 20040614-17; Vienna(AT) >EFFECT OF CORIOLIS AND CENTRIFUGAL FORCES ON TURBULENCE AND HEAT TRANSFER AT HIGH ROTATION AND BUOYANCY NUMBERS IN A RIB-ROUGHENED INTERNAL COOLING CHANNEL
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EFFECT OF CORIOLIS AND CENTRIFUGAL FORCES ON TURBULENCE AND HEAT TRANSFER AT HIGH ROTATION AND BUOYANCY NUMBERS IN A RIB-ROUGHENED INTERNAL COOLING CHANNEL

机译:肋骨强化内部冷却通道中高转速和浮力数时微孔和离心力对湍流和传热的影响

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摘要

Prediction of three-dimensional flow field and heat transfer in a two pass rib-roughened square internal cooling channel of turbine blades with rounded staggered ribs rotating at high rotation and density ratios is the main focus of this study. Rotation, buoyancy, ribs, and geometry affect the flow within these channels. The full two-pass channel with bend and with rounded staggered ribs with fillets (e/Dh =0.1 and P/e = 10) as tested by Wagner et. al [1992] is investigated. RSM is used in this study and enhanced wall treatment approach to resolve the near wall viscosity-affected region. RSM model was validated against available experimental data (which are primarily at low rotation and buoyancy numbers). The model was then used for cases with high rotational numbers (0.24, 0.475, 0.74 and 1) and high-density ratios (0.13, 0.23, and 0.3). Particular attention is given to how secondary flow, Reynolds stresses, turbulence intensity, and heat transfer are affected by coriolis and buoyancy/centrifugal forces caused by high levels of rotation and density ratios. A linear correlation for 4-side-average Nusselt number as a function of rotation number is derived.
机译:本研究的主要重点是对带有圆形交错肋肋的涡轮叶片的两遍肋肋粗化方形内部冷却通道中三维流场和传热的预测。旋转,浮力,肋骨和几何形状会影响这些通道内的流量。瓦格纳等人(Wagner et al。)测试了完整的两通通道,带有弯曲和带有圆角的圆角交错肋(e / Dh = 0.1,P / e = 10)。 al [1992]进行了研究。本研究中使用RSM和增强的壁处理方法来解决近壁粘度影响区域。针对可用的实验数据(主要是在低旋转数和浮力数下)验证了RSM模型。然后将该模型用于具有高旋转数(0.24、0.475、0.74和1)和高密度比(0.13、0.23和0.3)的情况。特别要注意的是二次流动,雷诺应力,湍流强度和传热如何受到高旋转率和密度比引起的科里奥利和浮力/离心力的影响。推导了4侧平均Nusselt数与旋转数的函数的线性相关性。

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