| 注册
首页|期刊导航|南京航空航天大学学报(英文版)|连续山丘地形上风力发电机功率输出特性数值分析

连续山丘地形上风力发电机功率输出特性数值分析

周天熠 谭剑锋 蔡建纲 史瑞鹏 夏云松

南京航空航天大学学报(英文版)2020,Vol.37Issue(1):120-128,9.
南京航空航天大学学报(英文版)2020,Vol.37Issue(1):120-128,9.

连续山丘地形上风力发电机功率输出特性数值分析

Numerical Investigation on Power Outputs of a Wind Turbine Sited over Continuous Hilly Terrain

周天熠 1谭剑锋 1蔡建纲 1史瑞鹏 1夏云松1

作者信息

  • 1. 南京工业大学机械与动力工程学院,南京 211816,中国
  • 折叠

摘要

Abstract

The location of wind turbines on a continuous hilly terrain has an influence on its power outputs. A CFD-based approach is developed to investigate the complex aerodynamic interference between two wind turbines and the hilly terrain. In this approach,a new three-dimensional model of hilly terrain is established to analyze its viscous effect,and a wind shear is modelled through logarithmic function. They are coupled into the aerodynamics of wind turbine based on"FLUENT"software. Then we apply the proposed method to the NREL Phase VI wind turbines and compare with an experiment in the atmospheric boundary layer(ABL)wind tunnel to validate its accuracy. The simulation also investigates the power outputs of wind turbines on the flat ground and the continuous hilly terrain by changing the location of the wind turbine related to the hilly terrain and the shape of the 1st hill. The results show that the wind turbine located on the top of the 2nd hill has the maximum power;and that when the wind turbine is located on the downstream of the hill,the stall zone should be avoided,and the power of the wind turbine located on the side of the hill is higher than that of the wind turbine located on the front and rear of the hilly terrain.

关键词

功率特性/风切变函数/NREL风力机/连续丘陵地形/仿真分析

Key words

power characteristics/wind shear function/NREL wind turbine/continuous hilly terrain/simulation analysis

分类

数理科学

引用本文复制引用

周天熠,谭剑锋,蔡建纲,史瑞鹏,夏云松..连续山丘地形上风力发电机功率输出特性数值分析[J].南京航空航天大学学报(英文版),2020,37(1):120-128,9.

基金项目

This work was supported by the Natu-ral Science Foundation of Jiangsu Province (No. BK20161537),National Science Key Laboratory Founda-tion(No.6142220180202),Rotor Aerodynamics Key Labo-ratory Foundation (No.RAL20180303-1),and National Natural Science Foundation of China(No.11502105). (No. BK20161537)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

访问量0
|
下载量0
段落导航相关论文