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Fusing Simulation Results From Multifidelity Aero-servo-elastic Simulators - Application To Extreme Loads On Wind Turbine

机译:多重航​​空伺服弹性模拟器融合仿真结果 - 应用于风力发电机组的极端负荷

摘要

Fusing predictions from multiple simulators in the early stages of the conceptual design of a wind turbine results in reduction in model uncertainty and risk mitigation. Aero-servo-elastic is a term that refers to the coupling of wind inflow, aerodynamics, structural dynamics and controls. Fusing the response data from multiple aero-servo-elastic simulators could provide better predictive ability than using any single simulator. The co-Kriging approach to fuse information from multifidelity aero-servo-elastic simulators is presented. We illustrate the co-Kriging approach to fuse the extreme flapwise bending moment at the blade root of a large wind turbine as a function of wind speed, turbulence and shear exponent in the presence of model uncertainty and non-stationary noise in the output. The extreme responses are obtained by two widely accepted numerical aero-servo-elastic simulators, FAST and BLADED. With limited high-fidelity response samples, the co-Kriging model produced notably accurate prediction of validation data.
机译:在风力涡轮机概念设计的早期阶段融合来自多个模拟器的预测可以减少模型的不确定性并降低风险。航空伺服弹性是一个术语,指的是风流入,空气动力学,结构动力学和控制的耦合。与使用任何单个仿真器相比,融合来自多个航空弹性仿真器的响应数据可以提供更好的预测能力。提出了从多保真航空伺服弹性模拟器融合信息的协同克里格方法。我们说明了协同克里格方法,该方法在输出中存在模型不确定性和非平稳噪声的情况下,将大型风力涡轮机叶片根部的极端襟翼弯曲力矩融合为风速,湍流和切变指数的函数。极端响应是通过两个广泛接受的数值气动-气动弹性模拟器FAST和BLADED获得的。在有限的高保真响应样本的情况下,协同克里格模型产生了验证数据的准确预测。

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