首页> 外文会议>American Society of Mechanical Engineers(ASME) Turbo Expo vol.3; 20040614-17; Vienna(AT) >LARGE EDDY SIMULATIONS OF FLOW AND HEAT TRANSFER IN ROTATING RIBBED DUCT FLOWS
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LARGE EDDY SIMULATIONS OF FLOW AND HEAT TRANSFER IN ROTATING RIBBED DUCT FLOWS

机译:旋转带肋管道流中流动和传热的大涡模拟

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Large eddy simulations are performed in a periodic domain of a rotating square duct with normal rib turbulators. Both the Coriolis force as well as the centrifugal buoyancy force are included in this study. A direct approach is presented for the unsteady calculation of the non-dimensional temperature field in the periodic domain. The calculations are performed at a Reynolds number (Re) of 12,500, a Rotation number (Ro) of 0.12 and an inlet coolant-to-wall density ratio (Δρ/ρ) of 0.13. The time-averaged Nusselt numbers compare satisfactorily with the data of Wagner et al. (J. Turbomachinery, Vol. 114, pp. 847-857). Time-sequences of the vorticity components and the temperature fields are presented to understand the flow physics and the unsteady heat transfer processes. Large scale coherent structures are seen to play an important role in the mixing and heat transfer. The temperature field appears to contain a low frequency mode that extends beyond a single inter-rib geometric module, and indicates the necessity of using at least two inter-rib modules for streamwise periodicity to be satisfied. Proper orthogonal decomposition (POD) of 200 snapshots indicates a low dimensionality of this system with almost 99% of turbulent energy in the first 80 POD modes.
机译:大涡模拟是在带有普通肋湍流器的旋转方管的周期域中执行的。这项研究包括科里奥利力和离心浮力。提出了一种直接方法来计算周期域中的无量纲温度场。在雷诺数(Re)为12,500,转数(Ro)为0.12和入口冷却剂与壁的密度比(Δρ/ρ)为0.13的情况下进行计算。时间平均Nusselt数与Wagner等人的数据令人满意。 (J.Turbomachinery,第114卷,第847-857页)。给出了涡度分量和温度场的时间序列,以了解流动物理学和不稳定的传热过程。可以看到大规模的相干结构在混合和传热中起着重要的作用。温度场似乎包含一个低频模式,该模式扩展到单个肋间几何模块之外,并表明必须使用至少两个肋间模块来满足流向周期性。正确的200次快照正交分解(POD)表示该系统的维数很低,在前80个POD模式中几乎有99%的湍流能量。

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