首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2010 >THE UNSTEADY PRESSURE SIGNATURE OF TRANSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION
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THE UNSTEADY PRESSURE SIGNATURE OF TRANSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION

机译:跨音速冲击波/边界层相互作用的非定常压力特征

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The statistics of wall pressure fluctuations beneathrna turbulent boundary layer interacting withrna normal shock wave are investigated exploitingrna direct numerical simulation (DNS) database. Inrnthe zero-pressure-gradient region upstream of therninteraction pressure statistics well compare withrncanonical boundary layers in terms of fluctuationrnintensities and frequency spectra. Pressure fluctuationsrnattain large values across the interactionrnzone, with an increase of about 7 dB from thernupstream level. The main effect of the interactionrnon the frequency spectra is to promote thernlow-frequency Fourier modes, and to inhibit thernhigh-frequency ones. Excellent collapse of frequencyrnspectra is observed past the interactionrnzone when data are scaled with the local boundaryrnlayer units. In this region an extended w?7/3rnpower-law behavior is observed, associated withrnthe suppression of mean shear caused by the imposedrnadverse pressure gradient.
机译:利用DNS直接数值模拟(DNS)数据库,研究了湍流边界层下方与正常冲击波相互作用的壁面压力波动的统计数据。在交互压力统计数据上游的零压力梯度区域,在波动强度和频谱方面,可以很好地与经典边界层进行比较。压力波动在整个相互作用区域内均达到较大值,与上游水平相比增加了约7 dB。相互作用与频谱的主要作用是促进低频傅里叶模式,并抑制高频模式。当使用局部边界层单位缩放数据时,观察到超过交互作用区的频谱会出现极好的崩溃。在该区域中观察到扩展的w?7 / 3rn幂律行为,与抑制由施加的负压梯度引起的平均剪切有关。

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