首页> 外文会议>International Mechanical Engineering Congress and Exposition >A COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF TURBULENCE AND WAKES OF HORIZONTAL AXIS WIND TURBINES DURING NON-OPERATIONAL TIME PERIODS
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A COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF TURBULENCE AND WAKES OF HORIZONTAL AXIS WIND TURBINES DURING NON-OPERATIONAL TIME PERIODS

机译:非运算期间水平轴风风力涡轮机湍流的计算流体动力学分析

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Wind turbines can create turbulence and downstream wakes which can introduce generation losses of downstream impacted turbines. These downstream turbine-induced losses are due to two different conditions. The first is from power-producing rotating blades of upstream wind turbines agitating the subsequent downstream wind in a cork-screw like manner. The second is from non-rotating, non-operational, non-power-generating wind turbines. These non-operating turbines may be under scheduled service shutdown, or rendered non-functional due to longer-term or permanent mechanical problems. In this work CFD was used to study downstream turbulence and wakes of a utility-scale, non-operational three-blade horizontal axis wind turbines (HAWT). A flow field was constructed using an unstructured grid around a HAWT (rotor hub elevation of 80 meters and a blade length of 40 meters). Various wind velocities were studied up to 25 meters per second. Incompressible flow was used to assess downstream turbulence using a three-dimensional steady state and unsteady state SST k-w (two equation) turbulence model. Different blade positions with respect to angle of attack (a) were studied, with a 4 degree angle of attack reported here. Pressures and velocities for distances of 100 meters in front and 500 meters downstream from the wind turbine are reported.
机译:风力涡轮机可以产生湍流和下游唤醒,这可以引入下游抗冲击涡轮机的产生损失。这些下游涡轮机诱导的损失是由于两个不同的条件。首先是从上游风力涡轮机的发电旋转刀片,使随后的下游风在类似于类似的方式的软木塞中。第二个是非旋转,非操作性的非发电风力涡轮机。这些非操作涡轮机可以在预定的服务关闭,或由于长期或永久的机械问题而呈现非功能性。在这项工作中,CFD用于研究公用事业尺度的下游湍流和唤醒,非操作的三刀片水平轴风力涡轮机(HAWT)。使用围绕HAWT(转子毂海拔80米的转子毂升高和40米的叶片长度)构建流场。各种风速速度高达25米,每秒25米。使用三维稳态和不稳定状态SST K-W(两个等式)湍流模型来利用不可压缩的流来评估下游湍流。研究了相对于攻击角度(a)的不同刀片位置,这里报告了4度的攻角。报告了前部100米的距离和500米处的距离的压力和速度。

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