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Parallel numerical simulations of subsonic, turbulent, flow-induced noise from two- and three-dimensional cavities using computational aeroacoustics.

机译:使用计算航空声学对二维和三维腔中亚音速,湍流,流动引起的噪声进行并行数值模拟。

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In this thesis, the phenomenon of flow-induced noise from two- and three-dimensional cavities is investigated with the use of computational aeroacoustics (CAA) and parallel computers. This is part of on-going research to further the current understanding of airframe noise. The field of CAA has shown great promise in the solution of primarily inviscid noise generation and wave propagation problems that are governed by the Euler equations. In the present study, these ideas are extended to the solution of the Navier-Stokes equations in multi-dimensions where the acoustic and flow fields may be influenced by viscous effects. A higher-order dual dual time-stepping algorithm is proposed in which efficient acceleration techniques typical of explicit steady-state solvers are extended to time-accurate calculations.; Flow over two-dimensional cavities with various geometric configurations, flow speeds, and types of incoming boundary layers are examined. For deep and moderately shallow cavities, the flow is oscillating in the shear layer mode. As the length-to-depth ratio of a two-dimensional cavity increases, the cavity flow is observed to oscillate in the wake mode. These phenomena are examined in detail. Correlation analyses of fluctuating pressure are carried out to estimate the convection speed of the large-scale structures, and the prediction is compared with experiment and theory. The use of a simple wall function at the upstream wall in order to alleviate the use of a full turbulent grid is assessed. Strouhal numbers of discrete tones at various subsonic speeds are compiled and compare with experimental data and direct numerical simulation. A simulation of flow-induced cavity noise over a three-dimensional cavity is performed at subsonic speeds and a low Reynolds number. Fluctuating flow quantities are averaged and compare with the mean experimental data. It is shown that three-dimensional calculations are necessary to simulate the correct physical behaviors of shallow cavities at subsonic speeds.
机译:本文利用计算航空声学(CAA)和并行计算机研究了二维和三维腔内流动引起的噪声现象。这是正在进行的研究的一部分,以进一步了解当前对机身噪声的了解。 CAA领域在解决主要由Euler方程控制的无形噪声产生和波传播问题方面显示出了巨大的希望。在本研究中,这些思想扩展到了多维和Navier-Stokes方程的解,其中,声学和流场可能受到粘性效应的影响。提出了一种高阶双对偶时间步长算法,其中将显式稳态求解器的典型有效加速技术扩展到了时间精确计算。检查具有各种几何构造,流速和进入边界层类型的二维腔体上的流动。对于深腔和中浅腔,流体以剪切层模式振荡。随着二维腔体的长深比增加,观察到腔体流在尾流模式下振荡。这些现象将详细检查。进行了脉动压力的相关分析,以估计大型结构的对流速度,并将其与实验和理论进行了比较。评估了在上游壁使用简单壁功能以减轻对整个湍流网格的使用的可能性。汇编了各种亚音速下离散声调的Strouhal数,并与实验数据和直接数值模拟进行了比较。在亚音速和低雷诺数下,对三维空腔上的流动引起的空腔噪声进行了仿真。对波动的流量进行平均,并与平均实验数据进行比较。结果表明,三维计算对于模拟亚音速下浅腔的正确物理行为是必要的。

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