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首页> 外文期刊>Modern Applied Science >Numerical Research on the Vortex Center on the Forward-Swept 3-D Wind Turbine Blades at Low Rotational Speed
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Numerical Research on the Vortex Center on the Forward-Swept 3-D Wind Turbine Blades at Low Rotational Speed

机译:低转速前掠3D风力涡轮机叶片涡中心的数值研究

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摘要

This paper studies the CFD simulation of forward three-dimensional (3-D) horizontal axis wind turbine (HAWT) blades. Using logarithmic grid and Q-criterion to learn the vortex dynamics around the blades at low rotational speed. The computational fluid dynamics (CFD) simulation uses Q-criterion to probe vortices and logarithmic grid to emphasize the micro-gridding effect of the turbulent boundary layer. The visualization and measurement of the simulation results give the coefficient of pressure (Cp). For forward 3-D wind turbine blade, at low rotational speed, the strongly accelerated laminar region surrounds the lower blade, and the decelerated tip blade region coalesce each other give rise to a reverse limiting streamline, eroding the laminar region further until a little is left on the tip of the blade. The reverse limiting streamline grows inward radially, the area is narrowing closing to the leading edge of the blade tip. The second side of the rolled-up vortex appears the velocity ratio (Uc/Ulocal) of the second vortices are higher than the main vortex cores. For radius R=1.547 m, U=12 m/s, at 210 RPM, CL and CD values reach a maximum with fully laminar tip conditions. While at 120 RPM, the CL and CD values reach a minimum in the absence of laminar tips. The results show the detailed vortex dynamic pattern surround the blades, give more understanding to design laminar 3-D blade toward a noiseless wind turbine system.
机译:本文研究了前向三维(3-D)水平轴风力涡轮机(HAWT)叶片的CFD仿真。使用对数网格和Q准则了解低转速下叶片周围的涡旋动力学。计算流体动力学(CFD)仿真使用Q准则探测涡旋和对数网格,以强调湍流边界层的微网格效应。仿真结果的可视化和测量给出了压力系数(Cp)。对于前向3-D风力涡轮机叶片,在低转速下,强烈加速的层流区域围绕下层叶片,而减速后的尖端叶片区域彼此结合会产生反向极限流线,从而进一步侵蚀层流区域,直至略微变窄。留在刀片的尖端。反向限制流线沿径向向内生长,该区域在靠近叶片尖端的前边缘处变窄。卷起的涡流的第二侧出现了第二个涡流的速度比(Uc / Ulocal)高于主涡流芯。对于半径R = 1.547 m,U = 12 m / s,在210 RPM时,在完全层流尖端条件下,CL和CD值达到最大值。当转速为120 RPM时,在没有层状尖端的情况下CL和CD值达到最小值。结果表明,围绕叶片的详细的涡流动力学模式,使人们更加了解将层状3-D叶片设计成无噪声的风力涡轮机系统。

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