TY - GEN
T1 - Aeroelastic behavior of offshore wind turbine airfoil during typhoon
AU - Ren, Nianxin
AU - Ou, Jinping
AU - He, Changjiang
PY - 2010
Y1 - 2010
N2 - In this paper, the aeroelastic behavior of the wind turbine FFA-W3-211 two-dimensional airfoil in the dynamic stall regime has been investigated during the natural typhoon real time history. What's more, the interaction between the airfoil stall-induced vibration and the unsteady flow has been effectively taken into consideration. Based on Navier-Stokes equation and k-ω SST turbulence model, the aerodynamic loads acting on the airfoil have been obtained by numerical simulation of the unsteady flow field near the airfoil under large angle of attack. Subsequently, the aerodynamic response of the airfoil can be calculated by embedding structural dynamics Newmark-β codes into the flow solver. Finally, the nonlinear interaction between the airfoil vibration and the unsteady flow can be successfully studied by taking advantage of the moving mesh technique for the simulation of the airfoil dynamic responses. Three kinds of stall-induced vibration have been considered: pitching oscillation, flap-wise oscillation and flap-pitching two degree-of-freedom coupled oscillation. Consequently, the key factors for the wind turbine two-dimensional airfoil aeroelastic performance during natural typhoon have been pointed out. Furthermore, the main reasons have been clarified in views of physical mechanism for fluid-structure interaction.
AB - In this paper, the aeroelastic behavior of the wind turbine FFA-W3-211 two-dimensional airfoil in the dynamic stall regime has been investigated during the natural typhoon real time history. What's more, the interaction between the airfoil stall-induced vibration and the unsteady flow has been effectively taken into consideration. Based on Navier-Stokes equation and k-ω SST turbulence model, the aerodynamic loads acting on the airfoil have been obtained by numerical simulation of the unsteady flow field near the airfoil under large angle of attack. Subsequently, the aerodynamic response of the airfoil can be calculated by embedding structural dynamics Newmark-β codes into the flow solver. Finally, the nonlinear interaction between the airfoil vibration and the unsteady flow can be successfully studied by taking advantage of the moving mesh technique for the simulation of the airfoil dynamic responses. Three kinds of stall-induced vibration have been considered: pitching oscillation, flap-wise oscillation and flap-pitching two degree-of-freedom coupled oscillation. Consequently, the key factors for the wind turbine two-dimensional airfoil aeroelastic performance during natural typhoon have been pointed out. Furthermore, the main reasons have been clarified in views of physical mechanism for fluid-structure interaction.
KW - Ffa-w3-211 airfoil
KW - Flap-pitching oscillation
KW - Fluid-structure interaction
KW - Stall-induced vibration
KW - Typhoon data
UR - https://www.scopus.com/pages/publications/77956280653
M3 - 会议稿件
AN - SCOPUS:77956280653
SN - 9781880653777
T3 - Proceedings of the International Offshore and Polar Engineering Conference
SP - 699
EP - 703
BT - Proceedings of the 20th (2010) International Offshore and Polar Engineering Conference, ISOPE-2010
T2 - 20th International Offshore and Polar Engineering Conference, ISOPE-2010
Y2 - 20 June 2010 through 25 June 2010
ER -