A two-way coupling method for the study of aeroelastic effects in large wind turbines

被引:22
|
作者
Della Posta, Giacomo [1 ]
Leonardi, Stefano [2 ]
Bernardini, Matteo [1 ]
机构
[1] Sapienza Univ Rome, Dept Mech & Aerosp Engn, I-00184 Rome, RM, Italy
[2] Univ Texas Dallas, Dept Mech Engn, Richardson, TX 75080 USA
关键词
Wind energy; Aeroelasticity; Large-eddy simulation; Actuator line model; Modal structural dynamics; CFD-CSD method; WAKE-INDUCED FATIGUE; DYNAMICS; TURBULENCE; COMPUTATIONS; SIMULATION; MODEL; SCALE; FLOW; CFD;
D O I
10.1016/j.renene.2022.03.158
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
The relevant size of state-of-the-art wind turbines suggests a significant Fluid-Structure Interaction. Given the difficulties to measure the phenomena occurring, researchers advocate high-fidelity numerical models exploiting Computational Fluid and Structural Dynamics. This work presents a novel aeroelastic model for wind turbines combining our Large-Eddy Simulation fluid solver with a modal beam-like structural solver. A loose algorithm couples the Actuator Line Model, which represents the blades in the fluid domain, with the structural model, which represents the flexural and torsional deformations. For the NREL 5 MW wind turbine, we compare the results of three sets of simulations. Firstly, we consider one-way coupled simulations where only the fluid solver provides the structural one with the aerodynamic loads; then, we consider two-way coupled simulations where the structural feedback to the fluid solver is made of the bending deformation velocities only; finally, we add to the feedback the torsional deformation. The comparison suggests that one-way coupled simulations tend to overpredict the power production and the structural oscillations. The flapwise blades vibration induces a significant aerodynamic damping in the structural motion, while the nose-down torsion reduces the mean aerodynamic forces, and hence the power, yet without introducing a marked dynamical effect. (c) 2022 Elsevier Ltd. All rights reserved.
引用
收藏
页码:971 / 992
页数:22
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