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Experimental Investigation of Reynolds Number Effect on Wind Turbine Profiles in the Cryogenic Wind Tunnel Cologne DNW-KKK 被引量:1

Experimental Investigation of Reynolds Number Effect on Wind Turbine Profiles in the Cryogenic Wind Tunnel Cologne DNW-KKK
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摘要 Wind turbine size has increased continuously and correspondingly also its Reynolds numbers. The Reynolds number effect can therefore no longer be ignored in design and optimization of wind turbines. Reliable profile test data should be available. A suitable facility for testing wind turbine profiles at high Reynolds numbers is the Cryogenic Wind Tunnel Cologne DNW-KKK. By means of injecting liquid nitrogen the tunnel can be cooled down to 100 K and the Reynolds number therefore can be raised accordingly. The maximum Reynolds number for 2D profile tests can reach 27x10^6. In this paper the test uncertainty and the flow quality of DNW-KKK were analyzed. Then some test results on the Reynolds number effect of the wind turbine profiles will be presented. The Reynolds number effect is different from model to model. Especially for thick profiles and flow control devices the Reynolds number effect is not always like the description in literature.
出处 《Journal of Energy and Power Engineering》 2013年第10期1957-1965,共9页 能源与动力工程(美国大卫英文)
关键词 Aerodynamics of wind turbine profiles Reynolds number effect cryogenic wind tunnel test. 风力发电机组 雷诺数效应 配置文件 低温风洞 科隆 风力涡轮机 测试数据 实验
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  • 1W.A. Timmer, R.P.J.O.M. van Rooij, Summary of the Delft University Wind Turbine Dedicated Airfoils, AIAA-2003-0352.
  • 2O. Ceyhan, Towards 20 MW wind turbine: High Reynolds number effects on rotor design, in: 50th AIAA Aerospace Sciences Meeting. Tennessee, USA, Jan. 2012.
  • 3F. Grasso, Usage of Numerical Optimization in Wind Turbine Airfoil Design, in: 28th AIAA Applied Aerodynamics Conference, Chicago, USA, June 28-July 1, 2010.
  • 4F. Grasso, Development of thick airfoils for wind turbines,in: 50th AIAA Aerospace Sciences Meeting, Nashville, TN, USA, Jan. 9-12, 2012.
  • 5H. Schlichting, E. Truckenbrodt, Aerodynamics of the Aeroplane, McGraw Hill Higher Education, 1979.
  • 6K. Freudenreich, K. Kaiser, A.P. Schaffarczyk, H. Winkler, R. Rebstock, Reynolds number and roughness effect on thick aerodynamic airfoils for wind turbines, Wind Engineering, Vol. 28, No. 5, 2005.
  • 7A.P. Schaffarczyk, H. Winkler, K. Freudenreich, K. Kaiser, R. Rebstock, Reynolds number effect on thick aerodynamic airfoils for wind turbines, in: European Wind Energy Conference and Exhibition, Madrid, Spain, June 2003.
  • 8W.A. Timmer, A.P. Schaffarczyk, The effect of roughness at high Reynolds numbers on the performance of DU-97-W300Mod, in: EWEC, Marseille, 2009.
  • 9R.P.J.O.M van Rooij, W.A. Timmer, Roughnesssensitivity considerations for thick rotor blade airfoils, AIAA-2003-0350.
  • 10R. Rebstock, Measurement techniques at high Reynolds numbers, in: 16th Symposium on Aerodynamics of Wind Turbines, Boulder, CO, USA, May 2003.

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