期刊文献+

APPLICATION OF CFD TECHNOLOGY IN WIND TURBINE ICING PROBER DESIGN 被引量:4

APPLICATION OF CFD TECHNOLOGY IN WIND TURBINE ICING PROBER DESIGN
下载PDF
导出
摘要 A series of numerical methods,which are suitable to design the shape and configuration of the icing prober for the horizontal axis wind turbine,are presented.The methods are composed of a multiple reference frame(MRF)method for calculating flow field of air,a Lagrangian method for computing droplet trajectories,an Eulerian method for calculating droplet collection efficiency,and an arithmetic for fast computing ice accretion.All the numerical methods are based on the computational fluid dynamics(CFD)technology.After proposing the basic steps and ideas for the design of the icing detection system,the shape and configuration of the icing prober for a 1.5 MW horizontal axis wind turbine are then obtained with the methods.The results show that the numerical methods are efficient and the CFD technology plays an important role in the design process. A series of numerical methods, which are suitable to design the shape and configuration of the icing prober for the horizontal axis wind turbine, are presented. The methods are composed of a multiple reference frame (MRF) method for calculating flow field of air, a Lagrangian method for computing droplet trajectories, an Eulerian method for calculating droplet collection efficiency, and an arithmetic for fast computing ice accretion. All the numerical methods are based on the computational fluid dynamics (CFD) technology. After proposing the basic steps and ideas for the design of the icing detection system, the shape and configuration of the icing prober for a 1.5 MW horizontal axis wind turbine are then obtained with the methods. The results show that the numerical methods are efficient and the CFD technology plays an important role in the design process.
出处 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2013年第3期264-269,共6页 南京航空航天大学学报(英文版)
关键词 wind turbine ice accretion computational fluid dynamics icing detection aerodynamic characteristics wind turbine ice accretion computational fluid dynamics icing detection aerodynamic characteristics
  • 相关文献

参考文献7

二级参考文献53

  • 1朱国林,M.Kronast.用二维N-S方程计算汽车流场的地面效应(英文)[J].空气动力学学报,1993,11(1):22-32. 被引量:22
  • 2易贤,朱国林.考虑传质传热效应的翼型积冰计算[J].空气动力学学报,2004,22(4):490-493. 被引量:17
  • 3张佃国,郭学良,付丹红,李宏宇.2003年8~9月北京及周边地区云系微物理飞机探测研究[J].大气科学,2007,31(4):596-610. 被引量:54
  • 4裘燮纲,韩凤华.飞机防冰系统[M].北京:航空专业教材编审组,1985.
  • 5Lynch F T, Khodadoust A. Effects of ice accretions on aircraft aerodynamics [J].Progress in Aerospace Sciences, 2001,37(8): 669-767.
  • 6Potapczuk M G. A review of NASA Lewis' development plans for computational simulation of aircraft icing[R]. AIAA-1999-243, 1999.
  • 7Bragg M B, Broeren A P, Blumenthal I. A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41(5): 323-362.
  • 8Cebeci T, Kafyeke F. Aircraft icing [J].Annual Review of Fluid Mechanics, 2003, 35: 11-21.
  • 9Hedde T, Guffond D. Development of a three-dimensional icing code-comparison with 3D experimental shapes[R]. AIAA-1992-41, 1992.
  • 10Hedde T, Guffond D. ONERA three dimensional icing model~J~. AIAAJournal, 1995, 36(6): 10:38-1045.

共引文献120

同被引文献27

  • 1朱国林,M.Kronast.用二维N-S方程计算汽车流场的地面效应(英文)[J].空气动力学学报,1993,11(1):22-32. 被引量:22
  • 2YAN L, KOTARO T, FANG F, et al. A wind tun- nel experimental study of icing on wind turbine blade airfoil E J]. Energy Conversion and Management, 2014,85(9) :591-595.
  • 3RHO M S. Atmospheric icing effects of aerodynam- ics of wind turbine blade [C]. Proceedings of the ASME 2013.
  • 4International Mechanical Engineering Congress and Exposition, IMECE2013-64085. [S. 1. ]: ASME, 2013.
  • 5OLIVIER P, ADRIAN I. Anti-icing and de-icing tech- niques for wind turbines Critical review[J]. Cold Re- gions Science and Technology, 2011,65(1) :88-96.
  • 6WRIGHT W B. Validation results for LEWICE 3.0 [R]. AIAA 2005-1243, 2005.
  • 7REID T, BARUZZI G, OZCER I. FENSAP-ICE simulation of icing on wind turbine blades[R]. Part 1= Performance Degradation, AIAA 2013-0750, 2013.
  • 8WOLFE H E, ANDERSEN W H. Kinetics, mecha- nism and resultant droplet sizes of the aerodynamic breakup of liquid drops= No. 0395-04 (18)SP[R]. California, USA, 1964.
  • 9LULIANO E, MINGIONE G,PETROSINO F. Eu- lerian modeling of large droplet physics toward realis- tic aircraft icing simulation[J]. Journal of Aircraft, 2011,48(5) .. 1621-1632.
  • 10WILLIAM W B, MARK G P. Semi-empirical mod- elin of SLD nhvsics[R].AIAA-2004-412. 2004.

引证文献4

二级引证文献4

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