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214 H. Guo et al.<br />

and “b” in Fig. 38.2b at α =40◦ , which correspond to the minimum and<br />

maximum lift, respectively. It can be observed from these pictures that:<br />

1. The flow around the airfoil is dominated by alternately rolling up and<br />

shedding of large vortices from leading and trailing edge. Laser sheet<br />

visualization reveals the separated shear layer rolling up into smaller<br />

vortices, smaller vortices amalgamating into a large vortex.<br />

2. Maximum lift occurs when the large vortex just formed from the leading<br />

edge and before its shedding downstream, as shown in Fig. 38.3b. The<br />

area occupied by this vortex is characterized by higher negative vorticity.<br />

When the minimum of the lift is reached, the large vortex evolves from<br />

the trailing edge, as shown in Fig. 38.3a.<br />

38.4 Conclusions<br />

This experimental study revealed that the second maximum lift at α ≈ 40 ◦ is<br />

induced by the large vortex developed from the amalgamation of the smaller<br />

vortices from the leading edge.<br />

References<br />

1. Wright A.K., Wood D.H., 2004, The starting and low wind speed behavior of a<br />

small horizontal axis wind turbine, Journal of <strong>Wind</strong> Engineering and Industrial<br />

Aerodynamics, 92: 1265–1279<br />

2. Wu J.Z., Lu X.Y., Denny A.G., Fan M., Wu J.M., 1998, Post-stall flow control<br />

on an airfoil by local unsteady forcing. Journal of Fluid Mechanics 371: 21–58<br />

3. Michos A., Bergeles G., Athanassiadis N., 1983, Aerodynamic Characteristics<br />

of NACA 0012 Airfoil in Relation to <strong>Wind</strong> Generators, <strong>Wind</strong> Engineering, 7:<br />

247–262<br />

4. Tangler J.L., 2004, Insight into a wind turbine stall and post-stall aerodynamics,<br />

<strong>Wind</strong> <strong>Energy</strong>, 7(3): 247–260

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