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An investigation of turbulence structure in a low Reynolds number incompressible turbulent boundary layer.

机译:低雷诺数不可压缩湍流边界层中的湍流结构研究。

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Hot-wire anemometry measurements in an incompressible turbulent boundary-layer flow over a flat plate at zero pressure gradient were made using two X-probes simultaneously. The experiment was performed in the large Atmospheric Boundary-Layer Wind Tunnel at the University of California, Davis. The 7.32 meter long flat plate installed within the wind tunnel generated approximately 20 cm thick boundary layer, with {dollar}Rsb{lcub}theta{rcub}{dollar} {dollar}approx{dollar} 4,000. Mean velocity and turbulence intensity data very close to the wall {dollar}(ysp{lcub}+{rcub} geq 1){dollar} were measured with a single hot wire to improve the measurement resolution. Space-time correlations of {dollar}uspprime{dollar} and {dollar}vspprime{dollar} velocities and of their instantaneous product were obtained with a pair of X-wires. The mean convection velocities, the extent in space, the mean inclination angles, and coherence characteristics of the {dollar}uspprime{dollar}, {dollar}vspprime{dollar} and {dollar}uspprime vspprime{dollar} large-scale structures are presented. (The {dollar}uspprime vspprime{dollar} results are presented for the first time.) The {dollar}uspprime{dollar} structure is inclined at a small angle (19{dollar}spcirc{dollar}) to the wall, while the {dollar}vspprime{dollar} and {dollar}uspprime vspprime{dollar} structures propagate almost at wall-normal directions. Each of the {dollar}uspprime{dollar} and {dollar}vspprime{dollar} structures appears elongated in the direction of the corresponding velocity fluctuation and is limited to {dollar}delta{dollar}-extent in the other two directions. The similarity between the {dollar}vspprime{dollar} and {dollar}uspprime vspprime{dollar} structures suggests that the {dollar}uspprime vspprime{dollar} might mainly be a consequence of the motion of the {dollar}vspprime{dollar} structure. Finally, a possible explanation for the differences between the {dollar}uspprime vspprime{dollar}, {dollar}vspprime{dollar} and the {dollar}uspprime{dollar} structures is the existence of different coherent structure scales, one dominating {dollar}uspprime{dollar} and the other dominating {dollar}vspprime{dollar} and {dollar}uspprime vspprime{dollar}.
机译:同时使用两个X探针在平板上以零压力梯度在不可压缩的湍流边界层流中进行热线风速测量。该实验是在加州大学戴维斯分校的大型大气边界层风洞中进行的。安装在风洞内的7.32米长平板产生约20厘米厚的边界层,其中{Rsb {lcub} theta {rcub} {dollar} {dollar}约{dollar}为4,000。用单根热线测量了非常接近壁{美元}(ysp {lcub} + {rcub} geq 1){美元}的平均速度和湍流强度数据,以提高测量分辨率。用一对X线获得了{usupprime {dollar}和{dollar} vspprime {dollar}速度及其瞬时乘积的时空相关性。给出了{dolus} uspprime {dollar},{dollar} vspprime {dollar}和{dollar} uspprime vspprime {dollar}大型结构的平均对流速度,空间范围,平均倾斜角度和相干特性。 (首次显示{dollar} uspprime vspprime {dollar}结果。){dollar} uspprime {dollar}结构相对于墙壁倾斜一小角度(19 {dollar} spcirc {dollar}),而{美元} vspprime {美元}和{美元} uspprime vspprime {美元}结构几乎在壁法线方向上传播。 {美元} uspprime {美元}和{美元} vspprime {美元}结构在相应速度波动的方向上显得拉长,并在其他两个方向上限制为{delta}美元。 {dollar} vspprime {dollar}和{dollar} uspprime vspprime {dollar}结构之间的相似性表明{dollar} uspprime vspprime {dollar}可能主要是{dollar} vspprime {dollar}结构运动的结果。最后,对于{dollar} uspprime vspprime {dollar},{dollar} vspprime {dollar}和{dollar} uspprime {dollar}结构之间差异的可能解释是存在不同的连贯结构尺度,其中一个主导的{dollar} uspprime {dollar}以及其他主导地位的{dollar} vspprime {dollar}和{dollar} uspprime vspprime {dollar}。

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