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Multivariate Statistics Analysis of the Pressure Field Induced by High-Speed Turbulent Boundary Layers

机译:高速湍流边界层引起的压力场的多元统计分析

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A DNS database of turbulent boundary layers with the freestream Mach number spanning from M_∞ = 2.5 to M_∞ = 14 is utilized to study multivariate statistics of pressure fluctuations induced by high-speed turbulent boundary layers. The multivariate pressure statistics include pressure correlations and coherence at multiple wall-normal locations, including those within the boundary layer and in the free stream. Within the boundary layer, the extent of pressure-correlation contours increases in both streamwise and spanwise directions as the wall-normal height increases, and variations in the freestream Mach number and the wall temperature do not seem to cause substantial differences in the size of large-scale pressure structures. In the free stream, however, the acoustic pressure structures exhibit a significant reduction in spatial length scales and structure angles as compared with those in the outer region of the boundary layer, and pressure wave fronts are found to be significantly shallower as Mach number increases. For all wall-normal locations, the coherence of pressure fluctuations attains much higher values at low frequencies and decays at high frequencies, with the spanwise coherence decaying substantially faster than the streamwise coherence. The coherence length increases with wall-normal coordinate within the boundary layer in both streamwise and spanwise directions. In the free stream, the streamwise coherence length and the Lagrangian correlation length are similar to those close to the wall, and such an apparent match indicates that the acoustic sources are located near the wall and is consistent with the 'Mach wave radiation' concept.
机译:利用自由流马赫数从M_∞= 2.5到M_∞= 14的湍流边界层DNS数据库来研究高速湍流边界层引起的压力波动的多元统计。多元压力统计数据包括多个壁法线位置(包括边界层和自由流内的法线位置)的压力相关性和相干性。在边界层内,随着壁法线高度的增加,压力相关轮廓的范围沿流向和跨度方向都增加,并且自由流马赫数和壁温的变化似乎不会引起大尺寸尺寸的实质性差异。规模的压力结构。然而,在自由流中,声压结构与边界层外部区域的声压结构相比,空间长度尺度和结构角度显着减小,并且随着马赫数的增加,声波波前明显变浅。对于所有壁面法线位置,压力波动的相干性在低频处均获得更高的值,而在高频处则衰减,而翼展方向的相干性的衰减速度远快于流态的相干性。相干长度在边界层内沿流向和展向随壁法向坐标增加。在自由流中,沿流的相干长度和拉格朗日相关长度类似于壁附近的长度,这种明显的匹配表明声源位于壁附近,并且与“马赫波辐射”的概念一致。

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