首页> 外文会议>ASME/JSME Joint Fluids Engineering Conference >NAVIER-STOKES ANALYSIS OF TIME-DEPENDENT FLOWS ABOUT WIND TURBINES
【24h】

NAVIER-STOKES ANALYSIS OF TIME-DEPENDENT FLOWS ABOUT WIND TURBINES

机译:Navier-Stokes关于风力涡轮机的时间依赖流的分析

获取原文

摘要

This paper presents an overview of an effort that uses various Reynolds-averaged Navier-Stokes (RaNS) methods to analyze time-dependent flows about horizontal-axis wind turbines (HAWT). The geometrically complex wind turbine consisting of closely coupled fixed and rotating components and complex flow phenomena including boundary-layer transition, unsteady tower wakes, and rotor-tower interaction make it an extremely difficult problem. The RaNS methods for this effort include a two-dimensional incompressible method and a three-dimensional compressible method. Both make use of structured overset grids to facilitate the simulation of flows about complex geometry. Boundary-layer transition can have a large effect on a wind turbine flowfield simulation. Several transition models including the classical Michel's method and the e n method were incorporated into the flow solvers. The e n method coupled to the Baldwin-Barth one-equation turbulence model shows good agreement with the wind-tunnel measured transition locations and loading characteristics for wind-turbine airfoils. Turbulent and unsteady tower wake affects wind-turbine rotor performance, aerodynamic loads, and acoustic characteristics. Two-dimensional studies demonstrate the capability to accurately model the tower's shedding frequency and resultant flow features. Unsteady, three-dimensional RaNS computation of the NREL Combined Experiment Phase II rotor demonstrates the capability, requirements and deficiency of current numerical methods. The current method captures the wake interactions between the rotor and tower and provides insight into the details of the wind-turbine flowfield.
机译:本文概述了使用各种雷诺平均的Navier-Stokes(RANS)方法来分析关于水平轴风力涡轮机(HAWT)的时间依赖流程的努力。由紧密耦合的固定和旋转部件和复杂的流动现象组成的几何复合风力涡轮机包括边界层过渡,不稳定塔唤醒和转子塔交互,使其成为极其困难的问题。该努力的RAN方法包括二维不可压缩方法和三维可压缩方法。两者都使用结构化的推销网格来促进流动仿真大约复杂几何形状。边界层过渡可以对风力涡轮机流场模拟具有很大的效果。包括典型米歇尔方法和E N方法的几种过渡模型掺入流动溶剂中。耦合到Baldwin-Barth一方程湍流模型的E N方法与风隧道测量的过渡位置和风力涡轮机翼型的负载特性显示了良好的一致性。湍流和不稳定的塔唤醒影响风力涡轮机转子性能,空气动力载荷和声学特性。二维研究证明了准确地模拟塔的脱落频率和所产生的流动特征的能力。不稳定,NREL组合实验期II转子的三维RAN计算表明了当前数值方法的能力,要求和缺乏。电流方法捕获转子和塔之间的唤醒相互作用,并向风力涡轮机流场的细节提供深入。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号