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Flow structure in a model of aircraft trailing vortices

机译:飞机尾涡模型中的流动结构

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摘要

We consider a model of incompressible trailing vortices consisting of an array of counter-rotating structures in a doubly periodic domain, infinite in the vertical direction. The two-dimensional vortex array of Mallier and Maslowe is combined with an axial velocity profile chosen proportional to the initial axial vorticity to provide an initial condition for the vortex wake. This base flow is a weak solution of the steady Euler equations with three velocity components that are functions of two spatial coordinates, thus allowing its linear stability properties to be investigated. These are used to interpret several stages in the development of vortex structure observed in fully three-dimensional direct numerical simulation (DNS) at Reynolds numbers Gamma/(2pinu)=[script O](1000). For sufficiently high axial velocity, its effect can be seen, in that each vortex in the linear array first develops helical structures before undergoing a period of relaminarization. At later times the more slowly growing cooperative elliptical instabilities become apparent, but the helical structure persists and the observed vortical structures remain coherent for longer periods than in the absence of axial velocity. Using the stretched-vortex subgrid model, large-eddy simulation runs are performed at large Reynolds numbers and a mixing transition identified at about Re=1–2×10^4. Similar phenomena are observed in these simulations as are seen in the DNS.
机译:我们考虑一个不可压缩的尾部涡流模型,该模型由一个在垂直方向上无限的双周期域中的反向旋转结构阵列组成。 Mallier和Maslowe的二维涡流阵列与选择的轴向速度曲线相结合,该速度与初始轴向涡度成正比,从而为涡流尾流提供了初始条件。该基流是具有两个空间坐标的函数的三个速度分量的稳态Euler方程的弱解,因此可以研究其线性稳定性。这些用于解释在雷诺数Gamma /(2pinu)= [script O](1000)的完全三维直接数值模拟(DNS)中观察到的涡旋结构发展的几个阶段。对于足够高的轴向速度,可以看到其效果,因为线性阵列中的每个涡旋在经历一定的层化之前首先会形成螺旋结构。在后来的时间里,合作椭圆的不稳定性变得越来越慢,但是与没有轴向速度的情况相比,螺旋结构仍然存在,并且观察到的涡结构在更长的时间内保持一致。使用拉伸涡流子网格模型,在大雷诺数下进行大涡模拟运行,并在大约Re = 1–2×10 ^ 4处确定混合过渡。在DNS中,在这些模拟中观察到了类似的现象。

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  • 作者

    Faddy J. M.; Pullin D. I.;

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  • 年度 2005
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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