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ERRATUM

Erratum: “Potential Load Reduction Using Airfoils with Variable Trailing Edge Geometry” [Journal of Solar Energy Engineering, 2005, 127(4), pp. 503–516] OPEN ACCESS

[+] Author and Article Information
Thomas Buhl, Mac Gaunaa, Christian Bak

J. Sol. Energy Eng 128(4), 580 (Nov 01, 2006) (1 page) doi:10.1115/1.2344829 History:
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Copyright © 2006 by American Society of Mechanical Engineers
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Figures

Grahic Jump Location
Figure 5

Inflow setup. The y=0 plane corresponds to the rotor plane. U corresponds to the rotational velocity, while V(t) corresponds to the free-stream velocity.

Grahic Jump Location
Figure 6

Deflection corresponding to β=5 deg. (a) Raw deflection shape. (b) Airfoil trailing edge region, with thickness.

Grahic Jump Location
Figure 7

Wind step response. Std(N) as a function of control parameter Ay.

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