D211 Experimental Study on Horizontal Axis Wind Turbine Generation System under Real Wind Condition System

2011 ◽  
Vol 2011.16 (0) ◽  
pp. 359-362
Author(s):  
Toshiyuki ASO ◽  
Katsuya IIDA ◽  
Tomoyuki AIDA ◽  
Akihiro UNNO ◽  
Yuuki HAYASHI ◽  
...  
Author(s):  
N S Tachos ◽  
A E Filios ◽  
D P Margaris

The analysis of the near and far flow fields of an experimental National Renewable Energy Laboratory (NREL) rotor, which has been used as the reference rotor for the Viscous and Aeroelastic Effects on Wind Turbine Blades (VISCEL) research program of the European Union, is described. The horizontal axis wind turbine (HAWT) flow is obtained by solving the steady-state Reynolds-averaged Navier—Stokes (RANS) equations, which are combined with one of four turbulence models (Spalart—Allmaras, k—∊, k—∊ renormalization group, and k—ω shear stress transport (SST)) aiming at validation of these models through a comparison of the predictions and the free field experimental measurements for the selected rotor. The computational domain is composed of 4.2×106 cells merged in a structured way, taking care of refinement of the grid near the rotor blade in order to enclose the boundary layer approach. The constant wind condition 7.2 m/s, which is the velocity of the selected experimental data, is considered in all calculations, and only the turbulence model is altered. It is confirmed that it is possible to analyse a HAWT rotor flow field with the RANS equations and that there is good agreement with experimental results, especially when they are combined with the k—ω SST turbulence model.


Wind Energy ◽  
2006 ◽  
Vol 9 (4) ◽  
pp. 361-370 ◽  
Author(s):  
Christophe Sicot ◽  
Philippe Devinant ◽  
Thomas Laverne ◽  
Stéphane Loyer ◽  
Jacques Hureau

2013 ◽  
Vol 291-294 ◽  
pp. 445-449
Author(s):  
De Shun Li ◽  
Ren Nian Li

Field experimental study is performed on a 33 kW horizontal axis wind turbine with rotor diameter of 14.8 m. The distribution of pressure is gathered by disposed 191 taped pressure sensors span-ward on seven particular sections of a blade. The results will provide a comparative basis to wind tunnel experiment and numerical calculation of the flow of the wind turbine.


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