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Assessment of turbulence models for the boundary layer transition flow simulation around a hydrofoil

机译:水翼轴上边界层过渡流模拟的湍流模型评估

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摘要

Boundary layer transition is a typical phenomenon in flows around hydrofoils and has a large influence on the hydrodynamic characteristics such as lift & drag, and vortex shedding. The purpose of this paper is to assess the predictive capability of different turbulence models in computational fluid dynamics (CFD) on boundary layer transition along a hydrofoil. Two typical sub-grid scale (SGS) stress models (LES WALE and LES Smagorinsky), as well as DDES gamma-Re-theta t, DDES, SSTCC gamma-Re-theta t, SST gamma-Re-theta t, and SST k-omega are selected. The boundary layer and wake flow calculated by different models are analyzed in detail and compared with the experimental data. The results show that large eddy simulation is more accurate than other models in terms of boundary layer velocity distribution, vortex shedding and wake structure prediction at the same grid conditions. The transition model considering curvature correction influences the predictive capability in the near-wall region compared with SST gamma-Re-theta t. The flow fields calculated by different curvature correction coefficients are quite different. In this paper, the prediction in the front of the transition end point (0.85L) has achieved good results as scaling coefficient is equal to 75 or 100. The transition model considering curvature modification improves the prediction of boundary layer transition by decreasing the turbulence intensity and increasing the pressure gradient of the aft part of the curvature hydrofoil leading. It is found that the LES model is the first choice in the case of enough computing resources. However, for engineering problems, it is highly efficient to adopt SSTCC gamma-Re-theta t model by adjusting the curvature correction coefficient.
机译:边界层转变是水翼仪周围流动的典型现象,对水动力学特性进行了大的影响,例如提升和阻力和涡旋脱落。本文的目的是评估在水翼沿边界层转换的计算流体动力学(CFD)中不同湍流模型的预测能力。两个典型的子网格刻度(SGS)应力模型(LES WALE和LES SMAGORINSKY),以及DDESγ-RE-THETA T,DDES,SSTCCγ-RE-THETA T,SST Gamma-RE-THETA T和SST k-omega被选中。通过不同模型计算的边界层和唤醒流程,并详细分析并与实验数据进行比较。结果表明,在边界层速度分布方面,大型涡流模拟比其他模型更准确,在相同的网格条件下涡旋脱落和唤醒结构预测。考虑曲率校正的转换模型影响与SSTγ-RE-THETA T相比的近壁区域中的预测能力。由不同曲率校正系数计算的流场非常不同。在本文中,过渡终点(0.85L)前面的预测已经实现了良好的结果,因为缩放系数等于75或100。考虑曲率修改的转换模型通过降低湍流强度来提高边界层转换的预测并提高曲率水膜的后部的压力梯度。发现LES模型是足够计算资源的第一选择。然而,对于工程问题,通过调整曲率校正系数来采用SSTCC Gamma-Re-Theta T模型来高效。

著录项

  • 来源
    《Ocean Engineering》 |2020年第2期|108124.1-108124.15|共15页
  • 作者单位

    China Agr Univ Coll Water Resources & Civil Engn Beijing 100083 Peoples R China|Eindhoven Univ Technol Dept Mech Engn NL-5600 MB Eindhoven Netherlands;

    China Agr Univ Coll Water Resources & Civil Engn Beijing 100083 Peoples R China;

    China Agr Univ Coll Water Resources & Civil Engn Beijing 100083 Peoples R China;

    Eindhoven Univ Technol Dept Mech Engn NL-5600 MB Eindhoven Netherlands;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    LES; Curvature; Hydrofoil; SSTCC; Boundary layer transition;

    机译:Les;曲率;水翼;SSTCC;边界层过渡;

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