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首页> 外文期刊>Measurement Science & Technology >Unsteady characteristics of near-wall turbulence using high repetition stereoscopic particle image velocimetry (PIV)
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Unsteady characteristics of near-wall turbulence using high repetition stereoscopic particle image velocimetry (PIV)

机译:使用高重复性立体粒子图像测速仪(PIV)的近壁湍流非稳态特征

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摘要

This study is part of a project that is aimed at building dynamic boundary conditions near a solid wall, in order to reduce the large eddy simulation spatial resolution that is necessary in this region. The objective is to build a low-order dynamical system in a plane parallel to the wall, which will mimic the unsteady behaviour of turbulence. This dynamical system should be derived from a POD decomposition of the velocity field. The POD decomposition is to be applied on an experimental database of time-resolved velocity fields. In order to obtain the experimental database, a specific experiment of high-speed stereoscopic particle image velocimetry (PIV) has been performed. This experiment was carried out in the turbulent boundary layer of the LML wind tunnel. The plane under study was parallel to the wall located at 100 wall units. This database is validated via comparison with hot-wire anemometry (HWA). Despite some peak locking observed on the streamwise velocity component, the PDF and the power spectra are in very good agreement with the HWA results. The two-point spatial correlations are also in good agreement with the results from the literature. As the flow is time-resolved, space-time correlations are also computed. The convection of the flow structure is observed to be the most important effect at this wall distance. The next step is to compute the dynamical system and to couple it to a large eddy simulation.
机译:这项研究是一个项目的一部分,该项目旨在在实体墙附近构建动态边界条件,以减少该区域所需的大涡流模拟空间分辨率。目的是在平行于壁的平面中构建一个低阶动力学系统,该系统将模拟湍流的不稳定行为。该动力学系统应源自速度场的POD分解。 POD分解将应用于时间分辨速度场的实验数据库。为了获得实验数据库,已进行了高速立体粒子图像测速(PIV)的特定实验。该实验是在LML风洞的湍流边界层中进行的。研究中的平面与位于100个墙单元处的墙平行。通过与热线风速仪(HWA)进行比较来验证该数据库。尽管在水流速度分量上观察到一些峰值锁定,但PDF和功率谱与HWA结果非常吻合。两点的空间相关性也与文献结果相吻合。由于流程是时间分解的,因此还计算了时空相关性。在此壁距下,观察到流动结构的对流是最重要的影响。下一步是计算动力系统,并将其耦合到大型涡流仿真中。

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