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Shed vortex structure and phase-averaged velocity statistics in symmetric/asymmetric turbulent flat plate wakes

机译:对称/非对称湍流平板唤醒的棚子涡旋结构和相平方速度统计

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The nearwake of a flat plate is investigated via direct numerical simulations. Many earlier experimental investigations have used thin plates with sharp trailing edges and turbulent boundary layers to create the wake. This results in large theta/D-TE values (theta is the boundary layer momentum thickness toward the end of the plate and D-TE is the trailing edge thickness). In the present study, the emphasis is on relatively thick plates with circular trailing edges (CTEs) resulting in theta/D values less than one (D is the plate thickness and the diameter of the CTE) and vigorous vortex shedding. The Reynolds numbers based on the plate length and D are 1.255 x 10(6) and 10 000, respectively. Two cases are computed: one with turbulent boundary layers on both the upper and lower surfaces of the plate (statistically the same, symmetric wake, Case TT) and the other with turbulent and laminar boundary layers on the upper and lower surfaces, respectively (asymmetric case, Case TL). The data and understanding obtained are of considerable engineering interest, particularly in turbomachinery where the pressure side of an airfoil can remain laminar or transitional because of a favorable pressure gradient and the suction side is turbulent. Shed-vortex structure and phase-averaged velocity statistics obtained in the two cases are compared here. The upper negative shed vortices in Case TL (turbulent separating boundary layer) are weaker than the lower positive ones (laminar separating boundary layer) at inception (a factor of 1.27 weaker in terms of peak phase-averaged spanwise vorticity at the first appearance of a peak). The upper vortices weaken rapidly as they travel downstream. A second feature of interest in Case TL is a considerable increase in the peak phase-averaged, streamwise normal intensity (random component) with increasing streamwise distance (x/D) that occurs near the positive vortex cores. This behavior is observed for a few diameters in the near wake. This is c
机译:通过直接数值模拟来研究平板的接近。许多早期的实验研究已经使用薄板,具有锋利的尾部边缘和湍流边界层以产生唤醒。这导致大的Theta / d-Te值(θ是朝向板末端的边界层动量厚度,D-Te是后缘厚度)。在本研究中,强调在具有圆形后缘(CTE)的相对厚的板上,导致小于一个(D是板厚度和CTE的直径)和剧烈的涡旋脱落。基于板长度和D的雷诺数分别为1.255×10(6)和10 000。计算出两种情况:板上的上表面和下表面上的湍流边界层(统计上相同,对称唤醒,情况TT),另一个分别在上表面和下表面上具有湍流和层边界层(不对称案例,案例TL)。所获得的数据和理解具有相当大的工程兴趣,特别是在涡轮机中,在翼型的压力侧可以保持层状或过渡,因为有利的压力梯度,吸力侧是湍流的。在此处比较两种情况下获得的血迹结构和相平均速度统计。上负棚涡流在情况TL(湍流分离边界层)比在一开始(1.27在第一次出现的一个因素在峰值相位平均翼展方向涡方面较弱下部正面的(层分离边界层)弱顶峰)。在下游旅行时,上涡流迅速削弱。壳体T1的兴趣的第二特征是峰值相位平均,流动正常强度(随机分量)的相当大的增加,其随着正涡流附近发生的流动距离(X / D)。在近似尾部的几总值中观察到这种行为。这是C.

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