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236 J.-L. Menet<br />

Fig. 43.1. 3D representation<br />

U<br />

θ<br />

d<br />

e<br />

e’<br />

Fig. 43.2. Savonius rotor<br />

U<br />

θ β<br />

e<br />

e9<br />

Fig. 43.3. Modified rotor<br />

43.2 Description of the Savonius Rotors<br />

The Savonius rotor is made from two vertical half-cylinders running around<br />

a vertical axis (Figs. 43.1, 43.2).<br />

A modified rotor (Fig. 43.3) is also studied, which is just an extrapolation<br />

of the Savonius rotor, using three geometrical parameters: the main overlap<br />

e, the secondary overlap e ′ , and the angle β between the paddles.<br />

In the following, we name conventional Savonius rotor the one for which<br />

the geometrical parameters e and e ′ are, respectively, equal to d/6 and 0. The<br />

characteristic curves of such a rotor (values of the power coefficient Cp and of<br />

the torque coefficient Cm towards the speed ratio λ) are presented in Fig. 43.4.<br />

43.3 Description of the Numerical Model<br />

The model used in this study is a mono-stepped rotor of infinite height. This<br />

hypothesis has allowed to carry out the calculations on the two-dimensional

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