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Optimum aerodynamic design for wind-lens turbine

机译:风镜涡轮的最佳空气动力学设计

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An optimum aerodynamic design method has been developed for the wind-lens turbine. The wind-lens turbine has a brimmed diffuser around a turbine rotor, which is referred to as wind-lens. The wind-lens can achieve the wind concentration on the turbine rotor, resulting in the significant enhancement of the turbine output. The present design method is based on a quasi-three-dimensional aerodynamic design method and a genetic algorithm. The quasi-three-dimensional design consists of two parts: a meridional viscous flow analysis and two-dimensional blade element designs. In the meridional viscous flow analysis, the axisymmetric Reynolds-averaged Navier-Stokes equations are numerically solved on a meridional plane to determine the wind flow rate through the wind-lens and the spanwise flow distribution at the rotor. The turbine rotor blade geometry is determined by the two-dimensional blade element theory based on the momentum theorem of the ducted turbine. The turbine rotor and wind-lens are simultaneously optimized by the present design method. Aerodynamic performance and flow fields in the optimum and conventional design cases have been investigated by wind tunnel tests and three-dimensional Reynolds-averaged Navier-Stokes simulations, in order to verify the effectiveness of the present design method. It is found that the optimum design case achieves the significant improvement in the output power coefficient, so that its numerical and experimental results of the output power coefficient exceed the Betz limit, which is the theoretical maximum output power coefficient for bare wind turbines. It is revealed that the aerodynamic matching between the turbine rotor and the wind-lens is essential to the performance enhancement of the wind-lens turbine.
机译:已经开发出用于风镜涡轮机的最佳空气动力学设计方法。风镜式涡轮机在涡轮机转子周围具有边缘扩散器,称为风镜。风镜可以使风聚集在涡轮转子上,从而显着提高涡轮输出。本设计方法基于准三维空气动力学设计方法和遗传算法。准三维设计包括两部分:子午粘性流分析和二维叶片单元设计。在子午流粘性分析中,轴对称的雷诺平均Navier-Stokes方程在子午面上进行数值求解,以确定通过风镜的风速和转子的翼展方向流量分布。涡轮机转子叶片的几何形状是基于导管式涡轮机的动量定理,通过二维叶片单元理论确定的。通过本设计方法同时优化了涡轮转子和风镜。为了验证本设计方法的有效性,已通过风洞试验和三维雷诺平均Navier-Stokes模拟研究了最佳和常规设计情况下的空气动力性能和流场。发现最优设计方案在输出功率系数方面取得了显着改善,因此其输出功率系数的数值和实验结果超过了Betz极限,这是裸机风力涡轮机的理论最大输出功率系数。揭示了涡轮转子和风镜之间的空气动力学匹配对于增强风镜涡轮的性能至关重要。

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