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Wall Pressure Signature in Compressible Turbulent Boundary Layers

机译:压缩湍流边界层的壁压特征

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Large-scale turbulent flow structures associated with positive and negative wall pressure fluctuations in a compressible turbulent boundary layer are investigated. Experiments are conducted in a closed-loop transonic wind tunnel at Ma = 0.5-0.8, Re_τ = 5,100-9,500 with combined velocity field and wall pressure measurements. Both, velocity and pressure statistics are analysed and compare well with existing low Mach number data. Spatial two-point correlation is applied to determine the size and orientation of the large-scale flow structures, which depending on the wall height have an averaged length scales of 4-6 δ and a maximum inclination angel of ≈ 12°-13°. The wall pressure fluctuations are associated with shear layer structures and it is shown that positive pressure fluctuations are correlated with low speed large-scale flow structures over streamwise extents of 4-5 δ.
机译:研究了与可压缩湍流边界层中的正壁压力波动相关的大规模湍流流量。实验在MA = 0.5-0.8的闭环跨音风隧道中进行,Re_τ= 5,100-9,500,综合速度场和壁压测量。分析速度和压力统计,并使用现有的低马赫数数据进行比较。施加空间两点相关性以确定大规模流动结构的尺寸和取向,这取决于壁高的平均长度为4-6δ和≈12°-13°的最大倾斜天使。壁压波动与剪切层结构相关,并且示出了正压波动与4-5δ的流动范围内的低速大型流动结构相关。

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