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Wake-tracking and turbulence modelling in computational aerodynamics of wind turbine aerofoils

机译:风力机翼型计算空气动力学中的尾迹跟踪和湍流建模

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This article addresses two modelling aspects of wind turbine aerofoil aerodynamics based on the solution of the Reynolds-averaged Navier-Stokes (RANS) equations. One of these is the effect of an a priori method for structured grid adaptation aimed at improving the wake resolution. The presented results emphasize that the proposed adaptation strategy greatly improves the wake resolution in the far field, whereas the wake is completely diffused by the nonadapted grid with the same number and spacing patterns of grid nodes. The proposed adaptation approach can be easily included in the structured generation process of both commercial and in-house-structured mesh generators. The other numerical aspect examined herein is the impact of particular choices for turbulence modelling on the predicted solution. This includes the comparative analysis of numerical solutions obtained by using different turbulence models, and also aims at quantifying the solution inaccuracy arising from not modelling the laminar-to-turbulent transition. It is found that the drag forces obtained by considering the flow as transitional or fully turbulent may differ by 50 per cent. All these issues are investigated using a special-purpose hyperbolic grid generator and two multi block structured finite volume RANS codes. The numerical experiments consider the flow field past a wind turbine aerofoil for which an exhaustive campaign of steady and unsteady experimental measurements was conducted. The predictive capabilities of the CFD solvers are validated by comparing experimental data and numerical predictions for selected flow regimes. The incompressible analysis and design code XFOIL is also used to support the findings of the comparative analysis of numerical RANS-based results and experimental data. [PUBLICATION ABSTRACT]
机译:本文介绍了基于雷诺平均Navier-Stokes(RANS)方程解的风力涡轮机翼型空气动力学的两个建模方面。其中之一是旨在改善唤醒分辨率的用于结构化网格自适应的先验方法的效果。提出的结果强调,所提出的自适应策略大大提高了远场中的唤醒分辨率,而唤醒则由具有相同数量和间隔模式的网格节点的非自适应网格完全扩散。所提出的自适应方法可以容易地包括在商用和内部结构化网格发生器的结构化生成过程中。本文研究的另一个数值方面是湍流建模的特定选择对预测解的影响。这包括通过使用不同的湍流模型获得的数值解的比较分析,并且还旨在量化由于不对层流到湍流过渡建模而产生的解误差。发现通过将流体视为过渡湍流或完全湍流而获得的阻力可能相差50%。所有这些问题都使用专用的双曲线网格生成器和两个多块结构的有限体积RANS代码进行了研究。数值实验考虑了经过风轮机翼型的流场,对此进行了详尽的稳态和非稳态实验测量。通过比较实验数据和选定流态的数值预测,可以验证CFD求解器的预测能力。不可压缩的分析和设计代码XFOIL也用于支持对基于RANS的数值结果和实验数据进行比较分析的结果。 [出版物摘要]

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