Abstract
An active flow control mechanism is proposed to improve the efficiency of the energy extraction for the vertical axis wind turbine. The proposed system consists of a vertical axis wind turbine with flexible blades. The conception is inspired from the vortex control mechanism utilized by the aero-/aqua animals to improve their performance via the flexion of their fins. The viscous non-stationary flow around the turbine is simulated using the ANSYS-FLUENT 15 software. The complex flapping motion is reproduced using a dynamic mesh technique and a user-defined function. The results show that, with this strategy of control, the turbine generates a higher moment coefficient due to the increase in the peaks of lift force caused by a better difference in the pressure between the two sides of the blade due to the flexure motion. The turbine power coefficient can reach 38 % enhancement for the optimal flow control conditions.
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Abbreviations
- A :
-
Rotor swept area
- a 0 :
-
Oscillating amplitude (m)
- C :
-
Blade chord (m)
- C L :
-
Lift coefficient
- \(C_{\text{D}}\) :
-
Drag coefficient
- \(C_{\text{m}}\) :
-
Moment coefficient
- \({\text{CP}}\) :
-
Power coefficient
- \(C_{\text{p}}\) :
-
Pressure coefficient
- \(D\) :
-
Turbine diameter (m)
- \(f\) :
-
Oscillating frequency (Hz)
- \(h(x)\) :
-
Instantaneous airfoil position along the x axis
- \(h(y)\) :
-
Instantaneous airfoil position along the y axis
- t :
-
Instant time (s)
- T :
-
Turbine revolution
- \(L\) :
-
Lift force (N)
- \(M\) :
-
Moment (N m)
- \(P\) :
-
Power (W)
- \(R\) :
-
Turbine radius (m)
- \(U\) :
-
Incoming flow velocity (m/s)
- LEV:
-
Leading edge vortex
- \({\text{zi}}\) :
-
Flapping frequency controlled parameter relative to turbine radius
- η :
-
Efficiency
- μ :
-
Dynamic viscosity
- ρ :
-
Density
- λ :
-
Tip speed ratio
- θ :
-
Turbine azimuthal angle (°)
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Technical Editor: Jose A. dos Reis Parise.
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Bouzaher, M.T., Hadid, M. & Semch-Eddine, D. Flow control for the vertical axis wind turbine by means of flapping flexible foils. J Braz. Soc. Mech. Sci. Eng. 39, 457–470 (2017). https://doi.org/10.1007/s40430-016-0618-3
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DOI: https://doi.org/10.1007/s40430-016-0618-3