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Abstract:
. I, u* @/ ]) e# z2 bAn aerodynamic model is development and coupled with a structural dynamic model. The BEM method with the modification of Du-Selig 3-D stall-delay model is adopted to calculate aerodynamic force. The structural dynamic model is an eighteen DOF rigid-elastic beam element including rigid displacements of flap, lag and pitch hinges. Finally, the aerodynamic model is verified and shows good agreement with experiment data.
/ M& O' m5 h- M8 J8 }" {8 b5 a. ?Keywords:aeroelasticity, aerodynamics, wind turbines |
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