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Abstract:
" C3 h% ` B5 X" O7 p: v% q$ CAn 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.1 o9 N/ S0 \ w, f& ]/ }
Keywords：aeroelasticity, aerodynamics, wind turbines |
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发表于 2008-11-5 09:06:48
