期刊文献+

动态风工况下复杂地形风电场流场多尺度仿真 被引量:5

MULTISCALE FLOW SIMULATION OF COMPLEX TERRAIN WIND FARM UNDER UNSTEADY WIND
原文传递
导出
摘要 首先在秒级风速数据的基础上构建动态风速函数模拟真实风速工况,同时基于高程数据构建某真实复杂地形的三维结构图。基于格子玻尔兹曼方法并结合自适应格子排布,对复杂地形风电场非定常流场进行数值计算,得到该风电场的风资源分布。之后在典型位置布置2台2 MW风力发电机,考虑真实风力机叶片的动态旋转计算风力机及真实复杂地形在动态风工况下的流场。研究实际复杂地形和动态风速下风电场的风速分布及尾流结构演变规律。结果表明:该方法可实现对复杂地形在动态来流风速作用下的风资源分布预测,并考虑风力机小尺度尾流结构实现对真实风电场流场的多尺度仿真。 A fitting function for the unsteady wind velocity based on the data measured several seconds apart is firstly developed,and the 3D structure of a real complex terrain in a wind farm is established according to the digital elevation model. Then,using the LatticeBoltzmann method(LBM)incorporated with the adaptive mesh refinement method,the unsteady flow field induced by the complex terrain is simulated and the distribution of wind energy resources is obtained. After that,the 2 MW wind turbines are sit in the wind farm and the full scale flow field induced by the terrain and wind turbines is simulated considering the rotating of blades. The wake structure of wind turbines in the complex terrain and under the unsteady inflow is investigated. The results show that the present modeling framework can be used to predict the wind resource distribution on the complex terrain considering the inflow velocity fluctuation,and achieve the multiscale simulation in a wind farm with considering the wake structure of wind turbines.
作者 李林敏 杨青 潘航平 Li Linmin;Yang Qing;Pan Hangping(National-Provincial Joint Engineering Laboratory for Fluid Transmission System Technology,Zhejiang Sci-Tech University,Hangzhou 310018,China;Zhejiang Aupu Co.,Ltd.,Hangzhou 311500,China;Zhejiang Windey Co.,Ltd.,Hangzhou 310012,China)
出处 《太阳能学报》 EI CAS CSCD 北大核心 2022年第11期179-185,共7页 Acta Energiae Solaris Sinica
基金 国家自然科学基金(52006197) 浙江省自然科学基金(LQ21E060012)。
关键词 风力发电机 风电场 数值模拟 格子玻尔兹曼方法 复杂地形 wind turbines wind farms computer simulation Lattice-Boltzmann method complex terrain
  • 相关文献

参考文献5

二级参考文献75

  • 1解福田,韩忠华,宋文萍.基于FW-Hpds方法的直升机旋翼气动噪声指向性分析[J].直升机技术,2007(1):11-15. 被引量:4
  • 2宋文萍,余雷,韩忠华.飞机机体气动噪声计算方法综述[J].航空工程进展,2010,1(2):125-131. 被引量:32
  • 3张兆顺,崔桂祥,徐春晓.湍流大涡模拟数值模拟的理论和应用[M].北京:清华大学出版社,2008.
  • 4F.Farassat,Jay H.Casper.Towards an airframe noise pre-diction methodology:survey of current approaches. 44th AI AA Aerospace Sciences Meeting and Exhibit . 2006
  • 5R.Khorrami,P.Lockard,M.Humphreys,et al.Preli mina-ry analysis of acoustic measurements fromthe nasa-gulfstream airframe noise flight. 14th AI AA/CEAS Aeroacoustics Conference . 2008
  • 6W.Stoker,Remy Gutierrez,V.Larssen,et al.High reyn-olds number aeroacoustic testing in NASA’s National Tran-sonic Facility(NTF). 46th AI AA Aero-space Sciences Meeting and Exhibit . 2008
  • 7Daniel Blacodon.Analysis of the airframe noise of an A320/A321with a parametric method. JOURNAL OF AIR-CRAFT . 2007
  • 8Gennaro Scarselli,Francesco Amoroso,Leonardo Lecce.Nu-merical si mulation,experi mental comparison with noise meas-urements and sound synthesis of airframe noise. 13th AI AA/CEAS Aeroacoustics Conference . 2007
  • 9Yueping Guo.A Semi-empirical model for aircraft landing gear noise prediction. 12th AIAA/CEAS Aeroacoustics Conference(27th AIAA Aeroacoustics Conference) . 2006
  • 10Yueping Guo.Adiscrete vortex model for slat noise prediction. 7th AI AA/CEAS Aeroacous-tics Conference . 2001

共引文献60

同被引文献48

引证文献5

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部