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Evolution of zero-pressure-gradient boundary layers from different tripping conditions

机译:不同脱扣条件下零压力梯度边界层的演变

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In this paper we study the spatial evolution of zero-pressure-gradient (ZPG) turbulent boundary layers from their origin to a canonical high-Reynolds-number state. A prime motivation is to better understand under what conditions reliable scaling behaviour comparisons can be made between different experimental studies at matched local Reynolds numbers. This is achieved here through detailed streamwise velocity measurements using hot wires in the large University of Melbourne wind tunnel. By keeping the unit Reynolds number constant, the flow conditioning, contraction and trip can be considered unaltered for a given boundary layer's development and hence its evolution can be studied in isolation from the influence of inflow conditions by moving to different streamwise locations. Careful attention was given to the experimental design in order to make comparisons between flows with three different trips while keeping all other parameters nominally constant, including keeping the measurement sensor size nominally fixed in viscous wall units. The three trips consist of a standard trip and two deliberately 'over-tripped' cases, where the initial boundary layers are over-stimulated with additional large-scale energy. Comparisons of the mean flow, normal Reynolds stress, spectra and higher-order turbulence statistics reveal that the effects of the trip are seen to be significant, with the remnants of the 'over-tripped' conditions persisting at least until streamwise stations corresponding to Re-x = 1.7 x 10(7) and x = O(2000) trip heights are reached (which is specific to the trips used here), at which position the non-canonical boundary layers exhibit a weak memory of their initial conditions at the largest scales O(10 delta), where delta is the boundary layer thickness. At closer streamwise stations, no one-to-one correspondence is observed between the local Reynolds numbers (Re-tau, Re-theta or Re-x etc.), and these differences are likely to be the cause of disparities between previous studies where a given Reynolds number is matched but without account of the trip conditions and the actual evolution of the boundary layer. In previous literature such variations have commonly been referred to as low-Reynolds-number effects, while here we show that it is more likely that these differences are due to an evolution effect resulting from the initial conditions set up by the trip and/or the initial inflow conditions. Generally, the mean velocity profiles were found to approach a constant wake parameter Pi as the three boundary layers developed along the test section, and agreement of the mean flow parameters was found to coincide with the location where other statistics also converged, including higher-order moments up to tenth order. This result therefore implies that it may be sufficient to document the mean flow parameters alone in order to ascertain whether the ZPG flow, as described by the streamwise velocity statistics, has reached a canonical state, and a computational approach is outlined to do this. The computational scheme is shown to agree well with available experimental data.
机译:在本文中,我们研究了零压力梯度(ZPG)湍流边界层从其起源到规范的高雷诺数状态的空间演化。主要动机是更好地了解在什么条件下可以以匹配的局部雷诺数在不同的实验研究之间进行可靠的标度行为比较。这是通过在大型墨尔本大学风洞中使用热线进行详细的沿流速度测量来实现的。通过保持单位雷诺数不变,对于给定的边界层的发展,可以认为流动调节,收缩和行程没有改变,因此可以通过移到不同的流向位置来独立于流入条件的影响来研究其演变。为了对三个不同行程的流量进行比较,同时保持所有其他参数的名义上恒定,包括将测量传感器的大小名义上固定在粘性壁单元中,对实验设计给予了认真的关注。这三个行程包括一个标准行程和两个故意的“超行程”情况,其中初始边界层被额外的大规模能量过度刺激。平均流量,正常雷诺应力,频谱和高阶湍流统计数据的比较表明,这次旅行的影响被认为是重要的,“过度旅行”条件的残留至少持续到与Re相对应的流向站为止。达到-x = 1.7 x 10(7)和x = O(2000)的行程高度(特定于此处使用的行程),在该位置非规范边界层在初始位置对初始条件的记忆力较弱最大尺度O(10 delta),其中delta是边界层的厚度。在更靠近水流的测站处,当地的雷诺数(Re-tau,Re-theta或Re-x等)之间未发现一对一的对应关系,这些差异可能是先前研究之间存在差异的原因。给定的雷诺数是匹配的,但不考虑行程条件和边界层的实际演变。在以前的文献中,这样的变化通常被称为低雷诺数效应,而在这里我们表明,这些差异更有可能是由于旅行和/或旅行设定的初始条件所导致的进化效应所致。初始流入条件。通常,随着沿测试区域的三个边界层的发展,发现平均速度剖面接近恒定的尾流参数Pi,并且发现平均流量参数的一致性与其他统计量也收敛的位置一致,包括高阶瞬间达到十阶。因此,该结果意味着,仅记录平均流量参数就足以确定流向速度统计数据所描述的ZPG流量是否已达到规范状态,为此概述了一种计算方法。计算方案显示与现有实验数据很好地吻合。

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