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一种风力机气动计算的全自由涡尾迹模型 被引量:5

A fully free vortex wake model of aerodynamic calculation for wind turbine
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摘要 采用全自由方式建立风力机尾流场的涡尾迹模型,引入"虚拟周期"的概念,并发展一种自适应松弛因子方法,从而改善了自由尾迹迭代的稳定性,提高了迭代收敛速度。利用建立的自由涡尾迹模型,计算了风力机叶片的尾流场结构、气动性能及叶片载荷,并与实验结果进行了对比分析。结果表明,尖速比越大,自适应松弛因子方法对缩小模型计算时间越有效;全自由涡尾迹模型能准确给出风力机尾流场的结构,包括尾迹的扩张以及叶尖涡和叶根涡的产生、发展和耗散的过程,风轮扭矩与实验数据吻合;叶片载荷分布的计算结果在低风速下与实验值基本一致,但是在大风速下差别较大,说明需要一个准确的失速模型。 A fully free vortex wake model of flow field and aerodynamic performance for wind turbine is presented.The dummy period concept is used to improve the convergence speed and stability of wake iterations with an introduction of the adaptive relaxation.The wake structure,the aerodynamic performance and loads of wind turbine are predicted by the present model and compared with the experiment results.The adaptive relaxation factor method can reduce the computational overhead especially at the high tip speed ratios.The fully free vortex wake model can accurately predict the flow field structure including wake expansion and the developing process from generation to dissipation of blade tip and root vortices.The rotor torque agrees well with the experiment data.As for blade load distribution,the calculation compares well with experiment at low wind speeds but diverges at high wind speeds,indicating that an appropriate stall model is required for accurate prediction at high speeds.
出处 《计算力学学报》 CAS CSCD 北大核心 2013年第6期822-827,共6页 Chinese Journal of Computational Mechanics
基金 国家自然科学基金(11172135) 国家科技支撑计划(2009BAA22B03) 江苏省优势学科建设工程 南京航空航天大学基本科研业务费专项科研(NJ2011003)资助项目
关键词 风力机 全自由涡尾迹 虚拟周期 自适应松弛 wind turbine fully free vortex wake dummy period adaptive relaxation
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  • 1胡丹梅,田杰,杜朝辉.水平轴风力机尾迹流场PIV实验研究[J].太阳能学报,2007,28(2):200-206. 被引量:30
  • 2Whale J, Anderson C G. An experimental investigation of wind turbine wakes using particle image velocimetry[c]//Proc 1993 European Community Wind Energy Conf, Germany: TravemuKnde, 1993:457-450.
  • 3Whale J, H.elmis C G, Papadopoulos K H, Anderson C G, Skyner D J. A study of the wake structure of a wind turbine comparing measurements from laboratory and full-scale experiments [J]. Solar Energy Engineering, 1995, 56(5):621-533.
  • 4Whale J, Anderson C G, Bareiss R, Wagner S. An experimental and numerical study of the vortex structure in the wake of a wind turbine [J].Journal of Wind Engineering and Industrial Aerodynamics, 2000, 84 ( 1 ) : 1-21.
  • 5Fujisawa N, Shibuya S. Observation of dynamic stall on Darrieus wind turbine blades[J]. Journal of Wind Engineering and Industrial Aerodynamics, 2001, 89 ( 2 ) : 201-214.
  • 6Hirahara H, Hossain M Z, Kawahashi M, Nonomura Y. Testing basic performance of a very small wind turbine designed for multi-purposes [J].Renewable Energy, 2005, 30 (8) : 1279- 1297.
  • 7Massouh F, Dobrev I. Exploration of the vortex wake behind of wind turbine rotor[J].Journal of Physics: Conference Series, 2007,75 : 012036. doi : 10. 1088/1742-6596/75/1/012036.
  • 8Hand M M, Simms D A, Fingersh L J, Jager D W, Cotrell J R, Schreck S, Larwood S M. Unsteady aerodynamics experiment phase VI : wind tunnel test configurations and available data campaigns[ R]. National Renewable Energy Laboratory, NREL/TP-500-29955, 2001.
  • 9Raffel M, Willert C, Wereley S, Kompenhans J. Particle Image Velocimetry: A Practical Guide[S]. 2nd ed. Berlin, Heidelberg, New Yowk: Springer, 2007.
  • 10Miller R H. Free wake techniques for rotor aerodynamic analysis--Volume 1 : summary of results and background theory[R]. NASA CR165434, 1982.

共引文献41

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  • 1李德源,叶枝全,陈严.风力机旋转叶片的多体动力学数值分析[J].太阳能学报,2005,26(4):473-481. 被引量:30
  • 2胡丹梅,田杰,杜朝辉.水平轴风力机尾迹流场PIV实验研究[J].太阳能学报,2007,28(2):200-206. 被引量:30
  • 3Landgrebe A. The wake geometry of a hovering rotor and its influence on rotor performanceI-J-:. Journal of the American Helicopter Society, 1972,17(4) : 2-15.
  • 4Kocurek J D,Tangler J L. A prescribed wake lifting surface hover performance analysisI-J]. Journal of the American Helicopter Society, 1977,22(1) : 24-35.
  • 5Egolf T A, Landgrebe A J. Helicopter rotor wake geometry and its influence in forward flight, vol. 1 generalized wake geometry and wake effects in rotor air loads and performancel-J3. NASA CR-3726,1983.
  • 6Coton F N, Wang T. The prediction of horizontal axis wind turbine performance in yawed flow using an un- steady prescribed wake modell-J]. Journal of Power and Energy, 1999,213 : 33-43.
  • 7Dumitrescu H, Cardos V. Wind turbine aerodynamic performance by lifting line method:J]. International Journal of Rotating Machinery, 1999,4(1) :141-149.
  • 8Kocurek D. Lifting Surface Performance Analysis for Horizontal Axis Wind Turbines[R]. Springfield: United States Department of Energy, 1987.
  • 9Sant T, Kuik G V, Bussel G J W. Estimating the angle of attack from blade pressure measurements on the NREL phase VI rotor using a free wake Vortex model: Axial conditions [J]. Wind Energy, 2006, 9:549-577.
  • 10Hansen M O L. Aerodynamics of Wind Turbines [M]. Earthsean,2"d edition,2008.

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