首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Assessing the Sensitivity of Stall-Regulated Wind Turbine Power to Blade Design Using High-Fidelity Computational Fluid Dynamics
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Assessing the Sensitivity of Stall-Regulated Wind Turbine Power to Blade Design Using High-Fidelity Computational Fluid Dynamics

机译:使用高保真计算流体动力学评估失速调节的风力涡轮机功率对叶片设计的敏感性

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摘要

This study provides a novel contribution toward the establishment of a new high-fidelity simulation-based design methodology for stall-regulated horizontal axis wind turbines. The aerodynamic design of these machines is complex, due to the difficulty of reliably predicting stall onset and poststall characteristics. Low-fidelity design methods, widely used in industry, are computationally efficient, but are often affected by significant uncertainty. Conversely, Navier-Stokes computational fluid dynamics (CFD) can reduce such uncertainty, resulting in lower development costs by reducing the need of field testing of designs not fit for purpose. Here, the compressible CFD research code COSA is used to assess the performance of two alternative designs of a 13-m stall-regulated rotor over a wide range of operating conditions. Validation of the numerical methodology is based on thorough comparisons of novel simulations and measured data of the National Renewable Energy Laboratory (NREL) phase VI turbine rotor, and one of the two industrial rotor designs. An excellent agreement is found in all cases. All simulations of the two industrial rotors are time-dependent, to capture the unsteadiness associated with stall which occurs at most wind speeds. The two designs are cross-compared, with emphasis on the different stall patterns resulting from particular design choices. The key novelty of this work is the CFD-based assessment of the correlation among turbine power, blade aerodynamics, and blade design variables (airfoil geometry, blade planform, and twist) over most operational wind speeds.
机译:这项研究为失速调节水平轴风力涡轮机的新型高保真仿真设计方法的建立提供了新的贡献。由于难以可靠地预测失速开始和失速特性,因此这些机器的空气动力学设计非常复杂。在行业中广泛使用的低逼真度设计方法虽然计算效率高,但通常会受到很大的不确定性的影响。相反,Navier-Stokes计算流体动力学(CFD)可以减少此类不确定性,并通过减少不适合用途的设计的现场测试需求来降低开发成本。在这里,可压缩的CFD研究代码COSA用于评估13m失速调节转子在广泛的运行条件下的两种替代设计的性能。数值方法的验证是基于对国家可再生能源实验室(NREL)第六阶段涡轮转子和两种工业转子设计之一的新型模拟和实测数据的全面比较。在所有情况下都可以找到很好的协议。两个工业转子的所有模拟都是时间相关的,以捕获与在大多数风速下发生的失速相关的不稳定。两种设计进行了交叉比较,着重​​于特定设计选择所导致的不同失速模式。这项工作的关键新颖之处在于,在大多数运行风速下,基于CFD的评估方法对涡轮功率,叶片空气动力学和叶片设计变量(机翼几何形状,叶片平面形状和扭曲)之间的相关性进行了评估。

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