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One-way fluid-structure interaction of a medium-sized heliostat using scale-resolving CFD simulation

机译:中尺度定日镜的单向流固耦合

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Vortex shedding and the resultant transient loadings on a medium-sized heliostat are investigated in this paper. Reynolds-Averaged Navier-Stokes (BANS) Computational Fluid Dynamics (CFD) of a simplified version of an operational heliostat, the LH-2, is used as a validation case for mean loads and to define the orientations used for fluid-structure interaction (FR): maximum drag in the upright position, and maximum torque-tube moment at an elevation of 60 degrees relative to the vertical. Optimized Atmospheric Boundary Layer profiles for mean flow and turbulence intensity were implemented as the inlet flow boundary condition for both the FLANS and Stress-Blended Eddy Simulation (SBES) simulations, with the latter using the synthetic turbulence technique, the Vortex Method, at the inlet. The SBES results show a strong likeness to the experimental results of Peterka et al. (1986) with a comparable mean and peak loading distribution. The transient SBES CFD pressure was implemented in a one-way FSI simulation to obtain the structural response of the heliostat to the transient wind loading. The results show that the response of the heliostat conformed to and depended on the mode shapes and frequencies of the heliostat structure more so than the vortex shedding frequencies. For the upright case, the Strouhal number obtained was within 8% of that obtained from an experimental study in literature, with the main vortex-shedding frequency shown to be 0.5 Hz. When excited with this wind, the structure responded with the third modal frequency of 2.7 Hz. The 60 degrees elevation case also responded mainly with the third mode of 2.6 Hz being excited, but the response was significantly influenced by a combination of higher modes located around 6 Hz. The results from the transient structural analysis using the temporal SBES heliostat surface pressure fields as input indicate that the method holds promise in predicting the transient response of heliostats. Importantly it can be concluded that due to the difference in frequencies between the vortex shedding and modal frequencies, the structure is safe from self-excitation.
机译:本文研究了中型定日镜上的涡旋脱落和由此产生的瞬态载荷。雷诺平均操作定日镜的简化版本LH-2的雷诺平均Navier-Stokes(BANS)计算流体动力学(CFD)用作平均载荷的验证案例并定义用于流体-结构相互作用的方向( FR):垂直位置的最大阻力,以及相对于垂直线60度仰角的最大扭矩管力矩。在FLANS和应力混合涡流模拟(SBES)模拟中,将用于平均流量和湍流强度的优化的大气边界层剖面作为入口流动边界条件,后者在入口处使用合成湍流技术(涡流方法) 。 SBES结果与Peterka等人的实验结果非常相似。 (1986年)的平均负荷和峰值负荷分布具有可比性。 SBES CFD瞬态压力是通过单向FSI模拟实现的,以获得定日镜对瞬态风荷载的结构响应。结果表明,定日镜的响应比涡旋脱落频率更符合并取决于定日镜结构的模式形状和频率。对于直立的情况,获得的斯特劳哈尔数在文献中的实验研究的结果的8%以内,主要的涡流脱落频率显示为0.5 Hz。当被这种风激发时,结构以2.7 Hz的第三模态频率响应。 60度仰角的情况也主要是通过激发2.6 Hz的第三模式做出响应,但是响应受到位于6 Hz左右的较高模式的组合的显着影响。使用临时SBES定日镜表面压力场​​作为输入的瞬态结构分析结果表明,该方法有望预测定日镜的瞬态响应。重要的是,可以得出结论,由于涡流脱落和模态频率之间的频率差异,该结构可避免自激。

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