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Numerical investigation of the aerodynamics and wake structures of horizontal axis wind turbines by using nonlinear vortex lattice method

机译:用非线性涡格法对水平轴风力机的空气动力学和尾流结构的数值研究。

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Wind turbines are emerging as one of the most promising and cost-effective renewable energy sources, due to their economical merits and technical maturity. It is important to accurately predict the aerodynamic performance of rotor blades for efficient design of wind turbine. Among the various numerical approaches, the vortex lattice method (VLM) is one of the most suitable models for wind turbine aerodynamics because the wind turbine mostly operates in the subsonic flow. However, it inherently cannot predict the nonlinear aerodynamic characteristics at a high angle of attack. In the current paper, a nonlinear vortex lattice method (NVLM) has been suggested to extend the existing VLM for handling the nonlinear stall and post-stall behaviors. This can be possible by finding a control point in the airfoil where the effective angle of attack is applied. This paper mainly discusses the development and validation of the NVLM for predicting the aerodynamic performances and the wake geometry against the measurements on the MEXICO rotor model. The comparison results show that the aerodynamic loads and tip vortex trajectories computed by NVLM are in significantly good agreement with the measured data. In addition, the complicated and unsteady wake structures are also analyzed using vortex particle method. (C) 2018 Elsevier Ltd. All rights reserved.
机译:由于风力涡轮机的经济优势和技术成熟度,它们正成为最有前途和最具成本效益的可再生能源之一。准确预测转子叶片的空气动力性能对于有效设计风力涡轮机非常重要。在各种数值方法中,涡流格子法(VLM)是最适合风力涡轮机空气动力学模型的模型之一,因为风力涡轮机主要在亚音速流中运行。但是,它固有地无法预测高攻角下的非线性空气动力学特性。在当前的论文中,提出了一种非线性涡旋格子法(NVLM)来扩展现有的VLM,以处理非线性失速和失速后的行为。这可以通过在机翼中找到一个施加有效迎角的控制点来实现。本文主要讨论了NVLM的开发和验证,以针对MEXICO转子模型上的测量结果预测空气动力性能和尾流几何形状。比较结果表明,NVLM计算出的空气动力载荷和叶尖涡旋轨迹与实测数据非常吻合。此外,还使用涡旋粒子法分析了复杂且不稳定的尾流结构。 (C)2018 Elsevier Ltd.保留所有权利。

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