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TURBULENT FLOW-FIELD COMPARISONS OF RANS AND LES FOR A TWISTED PIN LATTICE GEOMETRY AT LOW REYNOLDS NUMBER

机译:湍流流场比较RAN和LES在低雷诺数下扭销夹格几何形状

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The accurate evaluation of fuel and cladding peak temperatures is of prime importance for nuclear reactor design and safety. The Global Threat Reduction Initiative reactor conversion program often encounters exotic flow geometries in its mission to aid in converting reactors from high-enriched to low-enriched fuel. These geometries can pose modeling challenges. Analysis presented here concerns a reactor with twisted fuel pins that are in direct contact with each other in a large, hexagonal-pitch lattice. The Reynolds number for a unit cell is only 7500. Such flow conditions can present difficulties for standard approaches based on Reynolds-Averaged Navier-Stokes (RANS). Moreover there are no available experimental data and a small expected margin to the limiting cladding surface temperature. Given some of the geometric uncertainties, reducing the turbulence model uncertainty is thus important for meaningful calculations. A computational fluid dynamics model of a full-length unit cell was built using the commercial code STAR-CCM+. Multiple RANS models were employed, which gave disparate results. To provide higher-fidelity data for comparison, given the lack of experimental data, a periodic single-helical-pitch simulation with a Large Eddy Simulation (LES) approach was performed using Nek5000, a massively-parallel spectral-element code. This was compared with single-pitch RANS simulations from STAR-CCM+. Stream-wise velocity profile shape was generally well-represented by RANS. Cross-velocities and peak turbulent kinetic energy (TKE) were underestimated for most of the turbulence models with respect to LES, while mean flow TKE was universally underestimated. The overall results suggest that the Realizable k-ε Two-Layer model, which was the best at reproducing the LES TKE distribution, would likely be the most appropriate turbulence model choice for this flow. Future work includes full conjugate heat transfer simulations of 1/6 sectors of fuel assemblies featuring this type of pin lattice.
机译:准确评估燃料和包层峰值温度是核反应堆设计和安全性的重要性。全球威胁减少倡议反应堆转换计划经常在其使命中遇到异国情调的流动几何形状,以帮助将反应器转换为高富集的燃料。这些几何形状可能会造成建模挑战。这里提出的分析涉及一种具有扭曲燃料销的反应器,其在大的六边形桨级格中彼此直接接触。单位单元的雷诺数仅为7500.这种流动条件可能基于Reynolds平均的Navier-Stokes(RANS)对标准方法产生困难。此外,没有可用的实验数据和限制包层表面温度的小预期余量。考虑到一些几何不确定性,减少湍流模型的不确定性对于有意义的计算来说是重要的。使用商业代码Star-CCM +构建全长单元单元格的计算流体动力学模型。采用多次RAN模型,从而产生了不同的结果。为了提供更高保真数据以进行比较,鉴于缺乏实验数据,使用NEK5000进行具有大型涡流模拟(LES)方法的周期性单螺旋间仿真,是一种大规模并行谱元码。将其与来自Star-CCM +的单音rans模拟进行比较。流明智的速度曲线形状通常由RAN良好代表。对于大多数关于LES的大多数湍流模型,低估了横向速度和峰值湍流动能(TKE),而平均流量TKE普遍低估。总体结果表明,可实现的K-ε双层模型,这是再现LES TKE分布的最佳,这可能是该流动最适合的湍流模型选择。未来的工作包括完全共轭传热模拟的燃料组件的1/6扇区,具有这种类型的销格。

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