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Evidence of Surface Curvature Effects in Smooth Body Flow Separation Experiments

机译:光滑体流分离实验中表面曲率效应的证据

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This paper describes experiments on smooth body adverse pressure gradient (APG) turbulent boundary layer flow separation for the purpose of CFD validation and model development. The experimental geometry is designed to provide initial canonical turbulent boundary layer growth under nominally zero pressure gradient conditions prior to encountering a large, smooth, two-dimensional convex ramp geometry onto which a streamwise APG that is fully adjustable is imposed. Experiments encompassing both large-and small-scale smooth body flow separation as well as attached APG turbulent boundary layer development are realized on the same ramp geometry. The reported experiments are performed at M_∞ = 0.2 which corresponds to Re_θ ≈ 11,000 at the onset of the APG. Sample results are presented for the small-scale separation case and these include the evolution of both the mean flow and turbulent stresses at multiple spanwise locations on the ramp. Application of embedded shear layer scaling is shown to fully collapse the inflectional mean velocity profiles at all streamwise and spanwise locations on the ramp. When similar scaling is applied to the turbulent stresses, evidence of the effect of ramp surface curvature emerges. Due to the rapid transition from initially convex to concave curvature, it is demonstrated that the Reynolds stresses are effectively frozen.
机译:本文介绍了用于CFD验证和模型开发的光滑体逆压梯度(APG)湍流边界层流分离实验。实验几何设计成在遇到大的,平滑的,二维凸面斜坡几何形状之前,在名义上为零压力梯度的条件下,提供初始的规范湍流边界层生长,在该几何形状上施加完全可调的流式APG。在相同的坡道几何形状上实现了涵盖大型和小型平滑体流分离以及附加的APG湍流边界层展开的实验。报告的实验以M_∞= 0.2进行,相当于APG开始时的Re_θ≈11,000。给出了小规模分离情况的样本结果,其中包括在斜坡上多个翼展方向位置处的平均流量和湍流应力的演变。嵌入式剪切层定标的应用显示出可以完全消除斜坡上所有流向和跨度位置处的挠曲平均速度曲线。当对湍流应力应用类似的缩放比例时,就会出现斜坡表面曲率影响的证据。由于从最初的凸曲率迅速过渡到凹曲率,这证明了雷诺应力可以有效地冻结。

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