期刊文献+

两种自由尾迹模型在风力机气动性能预测中的应用 被引量:7

USING TWO FREE WAKE METHODS TO PREDICT THE AERODYNAMICS PERFORMANCE OF HAWT
下载PDF
导出
摘要 分别采用空间迭代法以及时间步进法的自由尾迹计算模型对风力机的尾迹进行预测。结合相应的算例以及模型特点预测风力机在正对来流、偏航以及变工况下的风力机尾迹形状并与相应的实验值进行比较。结果表明,在计算稳态工况时,空间迭代法可以快速稳定的预测出尾迹形状,而时间步进法在计算稳态工况时可以很好的收敛到初始值,而其瞬态特性保证该方法可以计算风力机在变工况下的气动特性。两种方法得到的尾迹形状基本反映叶尖涡结构的特性,可以用来作为升力线、升力面等工程模型算法的尾迹部分,用以进行水平轴风力机的气动性能预测。 Two different methods of free wake were used to predict the aerodynamics performance of horizontal axis wind turbine. Both wake model combined with certain blade model were then used to predict the geometry of the tip vortex of the wind turbine and the airloads of the blade for a wind turbine tested under certain control condition. It has been showed that relaxation free wake model can help to improve the stability characteristics of the scheme and enhance the convergence under steady state working eondition and the time-marching method can accurately predict the transient wake geometry to obtain accurately the unsteady airloads and power output of the wind turbine.
出处 《太阳能学报》 EI CAS CSCD 北大核心 2010年第7期923-927,共5页 Acta Energiae Solaris Sinica
基金 国家自然科学基金(50576052) 博士点基金(0060248036)
关键词 自由尾迹 空间迭代 时间步进 水平轴风力机 free wake relaxation time-marching wind turbine
  • 相关文献

参考文献13

  • 1Leishman J G.Principles of helicopter aerodynamics[M].Cambridge University Press,2006.
  • 2王适存,徐国华.直升机旋翼空气动力学的发展[J].南京航空航天大学学报,2001,33(3):203-211. 被引量:61
  • 3Lomax H,Pulliam T H,et al.Fundamentals of computational fluid dynamics[M].Springer Verlag,2001,85-190.
  • 4Miller R H.A simplified approach to the free wake analysis of a hovering rotor[J].Vertica,1982,6:89-95.
  • 5Bliss D B,Quackenbush T R,Bilanin A J.A new methodology for helicopter free-wake analyses[A].Proceedings of the 39th Annual National Forum of the American Helicopter Society[C],St Louis,MO,1983,9-11.
  • 6Bagai A,Leishman J G.Rotor free-wake modeling using a pseudoimplicit relaxation algorithm[J].Journal of Aircraft,1995,32(6):1276-1285.
  • 7Crimi P.Theoretical prediction of the flow in the wake of a helicopter roto[R].Cornell Aeronautical Laboratory Report,1965,BB-1994-5-1.
  • 8Scully M.A method of computing helicopter vortex wake distortion[R].Massachusetts Institute of Technology Report,1967,ASRLTR 138-1.
  • 9Egolf T,Massar J P.Helicopter free wake implementation on advanced computer architectures[A].2nd International Conference on Basic Rotorcraft Research[C],College Park,MD,Feb.1988,16-18.
  • 10Bhagwat M J,Leishman J G.Stability,consistency and convergence of time-marching free-vortex rotor wake algorithms[J].American Helicopter Society,2001,46(1):59-71.

二级参考文献9

共引文献60

同被引文献75

  • 1刘雄,陈严,叶枝全.水平轴风力机气动性能计算模型[J].太阳能学报,2005,26(6):792-800. 被引量:105
  • 2汪建文,贾瑞博,吴克启.风力机叶尖加小翼动力放大特性的数值模拟研究[J].太阳能学报,2007,28(1):55-61. 被引量:15
  • 3Leishman J G. Principles of helicopter aerodynamics [M]. New York: Cambridge University Press, 2006: 598-626.
  • 4Sandeep Gupta. Development of a time-accurate viscous Lagrangian vortex wake model for wind turbine applications[D]. Maryland: University of Maryland, College Park, 2006.
  • 5Leishman J G. Challenges in modelling the unsteady aerodynamics of wind turbines[J]. Wind Energy, 2002, 5(11): 85-132.
  • 6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.
  • 7National Advisory Committee for Aeronautics. The lift distribution of swept-blade winds [R]. Weissinger J, Washington : National Advisory Committee for Aeronautics, 1947.
  • 8Carr L W. Progress in the analysis and prediction of dynamic stall[J]. Journal of Aircraft, 1988, 25(1): 6-17.
  • 9Leishman J G, Beddoes T S. A semi-empirical.model for dynamic stall[J]. Journal of the American Helicopter Society, 1989, 34(3): 3-17.
  • 10Bagai A, Leishman J G. Rotor free-wake modeling using a pseudo-implicit algorithm[J]. Journal of Aircraft, 1995, 32(6): 1276-1285.

引证文献7

二级引证文献37

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