期刊文献+

基于升力面混合模型的水平轴风力机性能研究 被引量:1

A Study on the Performances of Wind Turbine with Horizontal Axis Based on the Hybrid Model of Actuator Surface
下载PDF
导出
摘要 提出了叶素方法(BEM)与升力面法相结合的一种新型混合模型.将叶片用一平面代替,并在叶片平面上采用压力跳跃边界条件,混合模型将CFD解算器与叶素方法(BEM)联合起来进行迭代求解,首先采用BEM模块根据入流条件和叶片各段面翼型的气动参数确定叶片上的不连续分布压力,然后采用CFD模型根据压力分布计算叶片上的力和转轮的流场尾迹结构等流场参数,CFD计算得到的流场参数再应用到BEM模块进行计算.每次迭代得到的流场参数与上次得到的值进行比较,残差达到要求则迭代过程结束.将该混合模型用于求解NREL第6期风力机出力性能,并与试验结果对比,得到了满意的效果. A hybrid model of the actuator surface combined with the blade element method (BEM) is presented. The blades are repIaeed by a mean surface and a "pressure jump" boundary condition is applied here. The hybrid model combines a CFD solver with the BEM. The solving method is iterative, at the beginning of iteration the BEM determines the pressure discontinuities along the blade span, using the rotor inflow and the aerodynamic properties of blade sections. Then the CFD solver applies this pressure discontinuity in order to model the blade forces and the wake downstream the rotor. The results were applied to the BEM module for the next calculation. At the end of iteration the obtained flow parameters and the residuals are compared with those obtained from previous iteration. If the required precision is attained, the calculation stops. Finally,the proposed hybrid model is used to calculate the performance of NREL Phase VI wind turbine and the results are satisfactory.
出处 《甘肃科学学报》 2009年第2期103-106,共4页 Journal of Gansu Sciences
基金 国家重点基础研究发展计划(973计划)课题(2007CB714602)
关键词 升力面 动量叶素理论 混合模型 风力机 性能 actuator surfaee BEM hybrid model wind turbine performance
  • 相关文献

参考文献8

  • 1杨瑞,李仁年,张士昂,李德顺.水平轴风力机CFD计算湍流模型研究[J].甘肃科学学报,2008,20(4):90-93. 被引量:9
  • 2杨瑞,李仁年,李银然,陈晓明.旋转效应对风力机叶片升力性能影响的研究[J].甘肃科学学报,2009,21(1):105-109. 被引量:1
  • 3Sorensen J and Shen W. Numerical Modeling of Wind Turbine Wakes[J]. Journal of Fluids Engineering, 2002,124 : 393-399.
  • 4Mikkelsen R. Actuator Disc Methods Applied to Wind Turbines [D]. Copenhagen:Technical University of Denmark,2003.
  • 5Hand M, Simms D, Fingersh L J, et al. Unsteady Aerodynamics Experiment Phase Ⅵ: Wind Tunnel Test Configurations and Available Data Campaigns[R]. NREL/TP-500-29955,2001.
  • 6Schmitz, S. , Chattot, J. J. Wind Turbine Blade Aerodynamics of the NREL Phase VI Rotor near Peak Power[A]. AIAA- 2005-4850,23rd AIAA Applied Aerodynamics Conference[C]. Toronto, 2005.
  • 7Schmitz S, Chattot J J. A Parallelized Coupled Navier-Stokes/ Vortex-Panel Solver[J]. Journal of Solar Energy Engineering, 2005,127:475-487.
  • 8Menter F R, Langtry R, Voelker S. Transition Modeling for General Purpose CFD Codes[A]. 6th International Symposium on Engineering Turbulence Modeling and Measurements, Sardinia[C]. ,2005.

二级参考文献17

  • 1杨瑞,李仁年,张士昂,李德顺.水平轴风力机CFD计算湍流模型研究[J].甘肃科学学报,2008,20(4):90-93. 被引量:9
  • 2Chaviaropoulos, PK, Hansen. Investigating 3D and Rotational Effects on Wind Turbine Blades by Means of a Quasi-3D Navier-Stokes Solver [J]. ASME Journal of Fluids Engineering, 2004,122 (2) : 330-336.
  • 3Xu,G. ,Sankar,L. Application of a Viscous Flow Methodology to the NREL Phase VI Rotor [A]. AIAA-2002-0030, 40th AIAA Aerospace Sciences Meeting and Exhibit[C]. Reno NV, 2002. NREL/TP-500-29 955.
  • 4Sφrensen, NN, Miehelsen, JA, Schreek, S. Navier Stokes Predictions of the NREL Phase Ⅵ Rotor in the NASA Ames 80ftx120ft Wind Tunnel[J]. Wind Energy, 2002,5 : 151-169.
  • 5Johansen,J, Sφrensen, N. N. Aerofoil Characteristics from 3D CFD Rotor Computations[J]. Wind Energy, 2004,7 (4) : 283- 294.
  • 6Gonzalez,A. Geometry and Rotational Effects on the Aerodynamic Behavior Using NREL UAE Data[A]. Proceedings of 45th AIAA Aerospace Sciences Meeting and Exhibit[C]. Reno, USA,January, 2007,20 (4) : 90-93.
  • 7Kuik, GAM van, Rooii , RPJOM van, Imamura, H. Analysis of the UAE Phase VI Wind Tunnel Results in the Non-yawed flow[A]. Proceedings of the 2004 European Wind Energy Conference and Exhibition on London[C]. London, November, 2004.
  • 8Benjanlrat, S. , Sankar, L. Recent Improvements to a Combined Navier-Stokes/Full-Potential Methodology for Modeling Horizontal Axis Wind Turbines[A]. AIAA-2004-0830,42nd AIAA Aerospace Sciences Meeting and Exhibit[C]. Reno NV,2004.
  • 9Hand MM, Simms DA, Fingersh LJ, Jager DW, Cotrell JR, Schreck S, Larwood SM. Unsteady Aerodynamics Experiment Phase Ⅵ:Wind Tunnel Test Configurations and Available Data Campaigns[R]. December, 2001.
  • 10[1]Hand MM.Simms DA,Fingersh LJ,et al.Unsteady Aerody-namlcs Experiment Phase Ⅵ:Wind Tunnel Test Configura-tions and Available Data Campaigns[R].December 2001,NREL/TP-500-29955.

共引文献8

同被引文献7

  • 1[法] D Le Gourieres风力机的理论与设计[M].施鹏飞译.北京:机械工业出版社,1987.
  • 2Fail P N Duque.Navier-Stokes Simulations of the Nrel Combined Experiment Phase Ⅱ Rotor[J].1999 European Wind Energy Comferendce.Nice:1999,79-84.
  • 3G E P Box,G M Jenkins.Times Series Analysis:Forecasting and Control[M].San Francisco:Holden-Day,1976.
  • 4Morino L,Kuo C C.Subsonic Potential Aerodynamics for Complex Configurations:Ageneral Theory[J].ALAA Jounral,1974,12(2):191-197.
  • 5Simiu E,Scanlan R H.Wind Effects on Structures:Fundamentals and Applications to Design[M].3rd Edition.New York:John Wiley & Sons Ltd.,1996.
  • 6张湘东,聂国华.大型水平轴风力机叶片气动性能优化[J].计算机辅助工程,2009,18(1):47-50. 被引量:9
  • 7阎超,谢磊,李云晓,赵小虎.翼型的气动最优化设计方法和反设计方法[J].空气动力学学报,1999,17(1):60-67. 被引量:14

引证文献1

二级引证文献3

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