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THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A DARRIEUS WIND TURBINE BLADE USING COMPUTATIONAL FLUID DYNAMICS AND LIFTING LINE THEORY

机译:基于计算流体动力学和升力线理论的达里乌斯风轮机三维气动分析

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Due to the rapid progress in high-performance computing and the availability of increasingly large computational resources, Navier-Stokes computational fluid dynamics (CFD) now offers a cost-effective, versatile and accurate means to improve the understanding of the unsteady aerodynamics of Darrieus wind turbines and deliver more efficient designs. In particular, the possibility of determining a fully resolved flow field past the blades by means of CFD offers the opportunity to both further understand the physics underlying the turbine fluid dynamics and to use this knowledge to validate lower-order models, which can have a wider diffusion in the wind energy sector, particularly for industrial use, in the light of their lower computational burden. In this context, highly spatially and temporally refined time-dependent three-dimensional Navier-Stokes simulations were carried out using more than 16,000 processor cores per simulation on an IBM BG/Q cluster in order to investigate thoroughly the three-dimensional unsteady aerodynamics of a single blade in Darrieus-like motion. Particular attention was payed to tip losses, dynamic stall, and blade/wake interaction. CFD results are compared with those obtained with an open- source code based on the Lifting Line Free Vortex Wake Model (LLFVW). At present, this approach is the most refined method among the "lower-fidelity" models and, as the wake is explicitly resolved in contrast to BEM-based methods, LLFVW analyses provide three-dimensional flow solutions. Extended comparisons between the two approaches are presented and a critical analysis is carried out to identify the benefits and drawbacks of the two approaches.
机译:由于高性能计算的飞速发展以及越来越多的计算资源的可用性,Navier-Stokes计算流体动力学(CFD)现在提供了一种经济高效,通用且准确的方法,以增进对Darrieus风的不稳定空气动力学的理解涡轮机,并提供更高效的设计。特别是,通过CFD确定通过叶片的完全解析的流场的可能性提供了机会,既可以进一步了解涡轮流体动力学的基础物理学,又可以利用该知识来验证低阶模型,该模型可以具有更广泛的应用范围。鉴于其较低的计算负担,其在风能领域的扩散,特别是工业用途。在这种情况下,在IBM BG / Q集群上,每次仿真使用16,000多个处理器核,进行了高度时空上随时间变化的三维Navier-Stokes仿真,以便全面研究飞机的三维非定常空气动力学。像Darrieus一样运动的单个刀片。特别注意了叶尖损失,动态失速和叶片/苏醒相互作用。将CFD结果与使用基于提升线自由涡流唤醒模型(LLFVW)的开源代码获得的结果进行比较。当前,此方法是“低保真”模型中最完善的方法,并且与基于BEM的方法相比,显着解决了尾流问题,因此LLFVW分析提供了三维流动解决方案。提出了两种方法之间的扩展比较,并进行了严格的分析,以确定这两种方法的优缺点。

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