Aeroelastic simulations of the DTU 10 MW turbine using tight coupling integration techniques

Konstantina Ntrelia, S. Vandewalle, J. Meyers
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引用次数: 0

Abstract

The present study aims to investigate a newly developed multirate time integration technique on aeroelastic simulations of the DTU 10 MW reference wind turbine inside a turbulent atmospheric boundary layer. The turbine is modelled using an actuator line model and a multibody structural solver is employed for the dynamic response. The turbine is studied under cases of laminar flow and a pressure driven boundary layer. Results show that the scheme exhibits high accuracy and matches the theoretical order of the Runge–Kutta scheme. During unsteady operations, substantial deformations were observed that are influenced mainly by the turbine’s rotation and the effect of turbulence in fatigue loading is highlighted.
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使用紧密耦合集成技术对 DTU 10 兆瓦涡轮机进行气动弹性模拟
本研究旨在研究一种新开发的多irate时间积分技术,用于模拟湍流大气边界层内 DTU 10 MW 参考风力涡轮机的气动弹性。涡轮机使用执行器线模型建模,并采用多体结构求解器进行动态响应。在层流和压力驱动边界层的情况下对涡轮机进行了研究。结果表明,该方案精度高,与 Runge-Kutta 方案的理论阶数相匹配。在非稳定运行期间,观察到了主要受涡轮机旋转影响的巨大变形,并强调了疲劳加载中湍流的影响。
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