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THE UNSTEADY PRESSURE SIGNATURE OF TRANSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION

机译:跨音频冲击波/边界层交互的不稳定压力签名

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The statistics of wall pressure fluctuations beneath a turbulent boundary layer interacting with a normal shock wave are investigated exploiting a direct numerical simulation (DNS) database. In the zero-pressure-gradient region upstream of the interaction pressure statistics well compare with canonical boundary layers in terms of fluctuation intensities and frequency spectra. Pressure fluctuations attain large values across the interaction zone, with an increase of about 7 dB from the upstream level. The main effect of the interaction on the frequency spectra is to promote the low-frequency Fourier modes, and to inhibit the high-frequency ones. Excellent collapse of frequency spectra is observed past the interaction zone when data are scaled with the local boundary layer units. In this region an extended w?7/3 power-law behavior is observed, associated with the suppression of mean shear caused by the imposed adverse pressure gradient.
机译:研究了与普通冲击波相互作用的湍流边界层下面的壁压波动的统计数据利用直接数值模拟(DNS)数据库。在相互作用压力统计的上游零压力梯度区域中,在波动强度和频谱方面与规范边界层进行比较。压力波动在相互作用区域上达到大值,从上游级别增加约7 dB。相互作用对频谱的主要效果是促进低频傅里叶模式,并抑制高频频率。使用本地边界层单元缩放数据时,观察到频谱的优异崩溃。在该区域中,观察到延长的W?7/3幂律行为,与由施加的不利压力梯度引起的平均剪切抑制相关联。

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