Load alleviation through adaptive trailing edge control surfaces: ADAPWING overview
暂无分享,去创建一个
[1] D. Weihs,et al. The Effect of Chordwise Flexibility on the Lift of a Rapidly Accelerated Airfoil , 1979 .
[2] J. Gordon Leishman,et al. Unsteady lift of a flapped airfoil by indicial concepts , 1994 .
[3] J. G. Leishman,et al. Unsteady aerodynamics of a flapped airfoil in subsonic flow by indicial concepts , 1995 .
[4] Berend G. van der Wall,et al. Experimental and Numerical Investigations on Steady and Unsteady Behaviour of a Rotor Airfoil with a Piezoelectric Trailing Edge Flap , 1999 .
[5] Torben J. Larsen,et al. Active load reduction using individual pitch, based on local blade flow measurements , 2005 .
[6] Mac Gaunaa,et al. Wind tunnel test on wind turbine airfoil with adaptive trailing edge geometry , 2007 .
[7] Christian Bak,et al. Potential load reduction using airfoils with variable trailing edge geometry , 2005 .
[8] Scott D. Collins,et al. Active Load Control for Airfoils using Microtabs , 2001 .