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An actuator sector method for efficient transient wind turbine simulation

机译:用于高效瞬态风力涡轮机仿真的执行器扇区方法

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摘要

This paper investigates a new method for transient simulation of flow through a wind turbine using an actuator technique. The aim, in the context of wind turbine wake simulation, is to develop an alternative to the widely used actuator disc model with an increased resolution and range of applications, for the same or less computational expense. In this new model, the actuator sector method, forces applied to the fluid are distributed azimuthally to maintain a continuous flow solution for increased time-step intervals compared with the actuator line method. Actuator sector results are presented in comparison with actuator disc and actuator line models initially for a non-dimensionalized turbine in laminar onset flow. Subsequent results are presented for a turbine operating in a turbulent atmospheric boundary layer. Results show significant increases in flow fidelity compared with actuator disc model results; this includes the resolution of diametric variation in rotor loading caused by horizontal or vertical wind shear and the helical vortex system shed from the turbine blade tips. Significant reductions in computational processing time were achieved with wake velocities and turbulence statistics comparable with actuator line model results. The actuator sector method offers an improved alternative to applications employing conventional actuator disc models, with little or no additional computational cost. This technique in conjunction with a Cartesian mesh-based parallel flow solver leads to efficient simulation of turbines in atmospheric boundary layer flows.
机译:本文研究了一种使用致动器技术对通过风力涡轮机的流动进行瞬态模拟的新方法。在风力涡轮机尾流仿真的背景下,其目的是以相同或更少的计算费用,开发出具有更高的分辨率和应用范围的,广泛使用的致动器盘模型的替代方案。在这种新模型中,执行器扇形方法将施加到流体上的力沿方位角分布,与执行器管线方法相比,可为增加的时间步长间隔保持连续的流动解。与最初用于无尺寸涡轮机的层流起始流中的执行器盘和执行器线模型进行比较,给出了执行器扇形结果。给出了在湍流大气边界层中运行的涡轮机的后续结果。结果表明,与执行器盘模型结果相比,流动保真度显着提高;这包括解决由水平或垂直风切变以及从涡轮机叶尖脱落的螺旋涡流系统引起的转子负载直径变化的解决方案。与执行器管线模型结果相比,苏醒速度和湍流统计数据显着减少了计算处理时间。执行器扇区方法为采用传统执行器盘模型的应用提供了一种改进的替代方法,几乎​​没有或没有额外的计算成本。结合基于笛卡尔网格的并行流求解器,该技术可以有效地模拟大气边界层流中的涡轮机。

著录项

  • 来源
    《Wind Energy 》 |2015年第4期| 699-711| 共13页
  • 作者单位

    Department of Engineering Science, The University of Auckland, Auckland 1142, New Zealand;

    Department of Mechanical Engineering, The University of Auckland, Auckland 1142, New Zealand;

    Department of Engineering Science, The University of Auckland, Auckland 1142, New Zealand;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    actuator sector; wind turbines; LES; wakes;

    机译:执行器部门;风力发电机;LES;唤醒;

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