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Turbulent Flow Induced Self-sustained Oscillations in Supersonic Cavity Flows

机译:超声速腔流中湍流引起的自持振荡

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The characteristics of self-sustained oscillations are investigated with high-resolution implicit large-eddy simulations of supersonic turbulent flow (M_∞=2.0) past a three-dimensional rectangular cavity with length-to-depth ratio of 2. First, the mechanism driving the self-sustained oscillations is verified to be a feedback-loop mechanism between the shear-layer instability and acoustics disturbances. The noise source in located near the trailing edge, and the generation of feedback compression waves is mainly related to the passage of vortices over the trailing edge. Second, the effects of the upstream boundary-layer thickness are analyzed. The upstream boundary-layer thickness has significant impacts on the features of noise radiation. As the upstream boundary-layer becomes thicker, the dominant mode of cavity tones is varied to a lower frequency, and a 8 dB decrease in sound pressure level is observed in the broadband noise radiation.
机译:通过超音速湍流(M_∞= 2.0)经过三维长径比为2的三维矩形腔的高分辨率隐式大涡模拟,研究了自持振荡的特性。自我维持的振动被证明是剪切层不稳定性和声学扰动之间的反馈回路机制。噪声源位于后缘附近,反馈压缩波的产生主要与涡流在后缘上的通过有关。其次,分析了上游边界层厚度的影响。上游边界层的厚度对噪声辐射的特征有重大影响。当上游边界层变厚时,腔体音调的主导模式将变为较低的频率,并且在宽带噪声辐射中观察到声压级降低了8 dB。

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