scholarly journals Simulation of oscillating trailing edge flaps on wind turbine blades using ranging fidelity tools

Wind Energy ◽  
2020 ◽  
Author(s):  
John M. Prospathopoulos ◽  
Vasilis A. Riziotis ◽  
Eva Schwarz ◽  
Thanasis Barlas ◽  
Maria Aparicio‐Sanchez ◽  
...  
2020 ◽  
Author(s):  
Prospathopoulos, John M. ◽  
Riziotis, Vasilis A. ◽  
Schwarz, Eva ◽  
Barlas, Thanasis ◽  
Aparicio-Sanchez, Maria ◽  
...  

2020 ◽  
pp. 0309524X2093885
Author(s):  
Farid Samara ◽  
David A Johnson

Due to the dynamic nature of the wind resource, wind turbine blades are subjected to significant variation in flow parameters, such as the angle of attack ([Formula: see text]). In some cases, the occurrence of dynamic stall on wind turbine blades causes load fluctuation which leads to material fatigue that tends to decrease the life span of the blades. In this study, the influence of a trailing edge flap on dynamic stall effects is investigated at high [Formula: see text] typical of wind turbines but atypical elsewhere. Pitching of the trailing edge flap was found to have a significant impact on the dynamic stall hysteresis loops responsible for the load fluctuation. Frequency analysis showed that the trailing edge flap was capable of reducing the cyclic fluctuation in the coefficient of lift and root bending moment by at least 26% and 24%, respectively. These results are a significant contribution toward understanding the advantages of using trailing edge flaps and how implementing them will reduce wind turbine blade load fluctuations.


Author(s):  
K. J. Standish ◽  
C. P. van Dam

The adoption of blunt trailing edge airfoils for the inner regions of large wind turbine blades has been proposed. Blunt trailing edge airfoils would not only provide increased structural volume, but have also been found to improve the lift characteristics of airfoils and therefore allow for section shapes with a greater maximum thickness. Limited experimental data makes it difficult for wind turbine designers to consider and conduct tradeoff studies using these section shapes. This lack of experimental data precipitated the present analysis of blunt trailing edge airfoils using computational fluid dynamics. Several computational techniques are applied including a viscous/inviscid interaction method and several Reynolds-averaged Navier-Stokes methods.


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