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Modified shear stress transport model with curvature correction for the prediction of swirling flow in a cyclone separator

机译:具有曲率校正的改进剪切应力传递模型用于预测旋风分离器中的旋流

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摘要

The paper investigates the confined swirling flow in a cyclone. The numerical simulations are performed using a proposed eddy viscosity turbulence model, which accounts for the effects of the streamline curvature and rotation. This distinguishes the current model from the conventional Eddy Viscosity Models (EVMs) that are known to fail to predict the Rankine vortex in swirling flows. Although computationally more expensive approaches, the Reynolds Stress Model (RSM) and Large Eddy Simulation (LES), have demonstrated a high capability of dealing with such flows, these techniques are often unsuited for use in complex design studies where computational speed and robustness are key factors. In the present approach, the Shear Stress Transport with Curvature Correction (SSTCC) turbulence model is modified by the introduction of the Richardson number to account for the rotation and curvature effects. The numerical predictions were validated using experimental results and also compared to the data obtained using the RSM model and various EVMs without the proposed modifications. The investigations started with a benchmark case of a flow through a channel duct with a U-turn, after which more challenging simulations of a high swirling flow within a cyclone separator device were performed. The results show that the proposed model is competitive in terms of accuracy when compared to RSM and proves to be superior to the RSM model in terms of computational cost. Furthermore, it is found that the proposed model preserves the ability to represent the Rankine vortex profile at different longitudinal levels of the cyclone. It is also more efficient in terms of the computational cost than the SSTCC model without the introduced modifications.
机译:本文研究了旋风分离器中的受限旋流。使用建议的涡流粘度湍流模型进行数值模拟,该模型考虑了流线曲率和旋转的影响。这将当前模型与传统的涡流粘度模型(EVM)区别开来,后者已知无法预测旋流中的朗肯涡旋。尽管在计算上更昂贵的方法(雷诺应力模型(RSM)和大涡模拟(LES))已显示出处理此类流的高能力,但这些技术通常不适合用于以计算速度和鲁棒性为关键的复杂设计研究中因素。在当前方法中,通过引入理查森数来修正旋转应力和曲率效应,从而修正了具有曲率校正的剪切应力传递湍流模型(SSTCC)。使用实验结果验证了数值预测结果,并将其与使用RSM模型和各种EVM(未经建议的修改)获得的数据进行了比较。研究从基准情况开始,该基准情况是通过带有U形转弯的通道管道进行的,然后对旋风分离器装置内的高涡流进行了更具挑战性的模拟。结果表明,与RSM相比,所提出的模型在准确性方面具有竞争力,并且在计算成本方面被证明优于RSM模型。此外,发现所提出的模型保留了在旋风器的不同纵向水平上代表朗肯涡旋分布的能力。在计算成本方面,它比没有引入修改的SSTCC模型更有效。

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