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Investigation of Subgrid-Scal Models in Large Eddy Simulation on the Unsteady Flow Around a Hydrofoil Using OpenFOAM

机译:基于OpenFOAM的水翼绕流非恒定流大涡模拟中的亚网格模型研究

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In this paper, we investigate the unsteady Reynolds-averaged Navier-Stokes simulations of the turbulent cavitating flow around a hydrofoil CLE. The primary objective of this study was to highlight the effect of subgrid-scale turbulence method in the prediction of unsteady vortical flow. In this work, the Smagorinsky and wall-adapting local eddy viscosity (WALE) models are selected to close the large eddy simulation equations. To investigate the limitations of these two models, the interactions between cavitation and vortices, the predicted streamlines, the velocities components, and the pressure oscillations have been discussed. The numerical results were compared with experimental results. These results showed that regardless of the selected turbulence model the development cycle of cavitation pocket is characterized by three levels: (first stage) the growth of attached pocket, (second stage) the separation of the attached pocket, and (last stage) the development and collapse of detached structures. The comparison between these two models shows that the WALE model takes into account both the rotation and strain rates, whereas the Smagorinsky model only takes into account the deformation rate of the turbulent structure. Besides, the WALE model is highly adaptive for wall-bounded flows. This advantage is explained by this ability to recover the near-wall scaling for the eddy viscosity. The WALE model has adopted a treatment without damping function or wall functions. Due to its algebraic nature, it offers a high-speed and efficient scheme compared to the Smagorinsky model. The study of the flow structures by iso-surface of the Q-criterion showed that the WALE model can predict the transition from laminar to the turbulent regime.
机译:在本文中,我们研究了绕水翼CLE的湍流空化过程的非稳态雷诺平均Navier-Stokes模拟。这项研究的主要目的是强调亚网格尺度湍流方法在预测非定常涡旋流动中的作用。在这项工作中,选择了Smagorinsky模型和与壁匹配的局部涡流粘度(WALE)模型,以关闭大型涡流仿真方程。为了研究这两种模型的局限性,讨论了空化和涡旋之间的相互作用,预测的流线,速度分量和压力振荡。将数值结果与实验结果进行了比较。这些结果表明,不管选择哪种湍流模型,空化穴的发展周期都具有以下三个特征:(第一阶段)附着穴的生长,(第二阶段)附着穴的分离和(最后阶段)发育和分离结构的崩溃。这两个模型之间的比较表明,WALE模型同时考虑了旋转速率和应变速率,而Smagorinsky模型仅考虑了湍流结构的变形速率。此外,WALE模型对壁垒流动具有高度的适应性。可以通过恢复涡流粘度的近壁结垢能力来解释这一优势。 WALE模型采用了无阻尼功能或无墙功能的处理方法。由于其代数性质,与Smagorinsky模型相比,它提供了一种高效的高速方案。通过Q准则的等值面对流动结构的研究表明,WALE模型可以预测从层流向湍流状态的过渡。

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