期刊文献+

Dynamic Loads and Wake Prediction for Large Wind Turbines Based on Free Wake Method 被引量:1

Dynamic Loads and Wake Prediction for Large Wind Turbines Based on Free Wake Method
在线阅读 下载PDF
导出
摘要 With large scale wind turbines,the issue of aerodynamic elastic response is even more significant on dynamic behaviour of the system.Unsteady free vortex wake method is proposed to calculate the shape of wake and aerodynamic load.Considering the effect of aerodynamic load,inertial load and gravity load,the decoupling dynamic equations are established by using finite element method in conjunction of the modal method and equations are solved numerically by Newmark approach.Finally,the numerical simulation of a large scale wind turbine is performed through coupling the free vortex wake modelling with structural modelling.The results show that this coupling model can predict the flexible wind turbine dynamic characteristics effectively and efficiently.Under the influence of the gravitational force,the dynamic response of flapwise direction contributes to the dynamic behavior of edgewise direction under the operational condition of steady wind speed.The difference in dynamic response between the flexible and rigid wind turbines manifests when the aerodynamics/structure coupling effect is of significance in both wind turbine design and performance calculation. With large scale wind turbines,the issue of aerodynamic elastic response is even more significant on dynamic behaviour of the system.Unsteady free vortex wake method is proposed to calculate the shape of wake and aerodynamic load.Considering the effect of aerodynamic load,inertial load and gravity load,the decoupling dynamic equations are established by using finite element method in conjunction of the modal method and equations are solved numerically by Newmark approach.Finally,the numerical simulation of a large scale wind turbine is performed through coupling the free vortex wake modelling with structural modelling.The results show that this coupling model can predict the flexible wind turbine dynamic characteristics effectively and efficiently.Under the influence of the gravitational force,the dynamic response of flapwise direction contributes to the dynamic behavior of edgewise direction under the operational condition of steady wind speed.The difference in dynamic response between the flexible and rigid wind turbines manifests when the aerodynamics/structure coupling effect is of significance in both wind turbine design and performance calculation.
出处 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2015年第2期240-249,共10页 南京航空航天大学学报(英文版)
基金 supported by the National Basic Research Program of China (973 Program) (No. 2014CB046200) the Jiangsu Province Natural Science Foundation (No.BK2012390) the Fundamental Research Funds for the Central Universities the Priority Academic Program Development of Jiangsu Higher Education Institutions
关键词 wind turbine free wake method aerodynamic dynamics structural dynamics wind turbine free wake method aerodynamic dynamics structural dynamics
作者简介 Corresponding author: Wang Tongguang, Professor, E-mail: tgwang@nuaa. edu. cn.
  • 相关文献

参考文献1

二级参考文献20

  • 1Leishman J G. Principles of helicopter aerodynamics [M]. New York: Cambridge University Press, 2006: 598-626.
  • 2Sandeep Gupta. Development of a time-accurate viscous Lagrangian vortex wake model for wind turbine applications[D]. Maryland: University of Maryland, College Park, 2006.
  • 3Leishman J G. Challenges in modelling the unsteady aerodynamics of wind turbines[J]. Wind Energy, 2002, 5(11): 85-132.
  • 4李春华.时间准确自由尾迹方法建模及(倾转)旋翼气动特性分析[D].南京:南京航空航天大学,2007.
  • 5National Advisory Committee for Aeronautics. The lift distribution of swept-blade winds [R]. Weissinger J, Washington : National Advisory Committee for Aeronautics, 1947.
  • 6Carr L W. Progress in the analysis and prediction of dynamic stall[J]. Journal of Aircraft, 1988, 25(1): 6-17.
  • 7Leishman J G, Beddoes T S. A semi-empirical.model for dynamic stall[J]. Journal of the American Helicopter Society, 1989, 34(3): 3-17.
  • 8Bagai A, Leishman J G. Rotor free-wake modeling using a pseudo-implicit algorithm[J]. Journal of Aircraft, 1995, 32(6): 1276-1285.
  • 9李清杨,关治,白峰杉.数值计算原理[M].北京:清华大学出版社,2000:356-407.
  • 10Bhagwat M J, Leishman J G. Generalized viscous vortex model for application to free-wake and aeroacoustic calculations[C]//58th Annual Forum and Technology Display of the American Helicopter Society International, Montreal, Canada, 2002.

共引文献8

同被引文献2

引证文献1

二级引证文献6

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