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Sound Generation in Plane Couette Flow: A Failure of Lighthill's Analogy

机译:飞机Coute Flow的声音产生:灯灰体的比喻失败

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The linear mechanism of acoustic wave generation by initially pure vortex perturbations embedded in a two-dimensional, inviscid and unbounded Couette flow is investigated by Kelvin-mode analysis and direct numerical simulations (DNS). Our results show a misleading representation of the linear sources of aerodynamic sound generation by Lighthill's acoustic analogy approach, not taking the strong anisotropy of the linear generation of acoustic waves by pure vortex mode perturbations in non-normal shear flow systems into account. DNS confirm the importance of linear sound production in the range of validity of rapid distortion theory (RDT), herein being superior compared to the nonlinear mechanism despite the common opinion.
机译:通过Kelvin-Mode分析和直接数值模拟(DNS)研究了嵌入二维,无粘性和未绑定的循环流动中嵌入二维,无粘性和未绑定的豆流程中的最初纯Vortex扰动的线性机制。 我们的结果表明,Lightill的声学类比方法的线性源的线性源的误导性表示,而不是在非正常剪切流量系统中通过纯涡流模式扰动进行线性产生的线性产生的强大各向异性。 DNS确认线性声音产生在快速变形理论(RDT)的有效范围内的重要性,这里与非线性机制相比,尽管存在共同点。

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