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Two-dimensional linear instability of a Lamb-Oseen counter-rotating vortex dipole

机译:Lamb-Oseen反向旋转涡旋偶极子的二维线性不稳定性

摘要

The present study investigates the stability of a family of quasi-steady two-dimensional vortex dipoles resulting from the adaptation to the mutual deformation and viscous diffusion of counter-rotating Lamb-Oseen vortices of equal size and circulation. For sufficiently large Reynolds numbers, the internal structure is set by the dipole aspect ratio a/b (radius versus separation distance), giving rise to a family of smooth quasi-steady solutions. These base flow solutions consist of self-propagating dipoles with a vorticity trail leaking from the dipole during the self-adaptation process and from diffusion across the dipole Kelvin oval. The present work is a generalization of the recent study by Brion et al. (2014), who found that a specific kind of vortex dipole, the Lamb-Chaplygin dipole, was unstable with respect to two-dimensionnal perturbations. We show how the growth rate and spatial structure of the unstable modes vary with aspect ratio a/b and Reynolds number. The growth rates are lower than for the Lamb-Chaplygin dipole and decreases when the aspect ratio is lowered. It is advocated here that these new two-dimensional modes of small aspect-ratio smooth dipoles are good candidates for steady actuation in aircrafts conditions.
机译:本研究调查了准反向二维Lamb-Oseen涡旋的相互变形和粘性扩散的适应所导致的准稳态二维涡旋偶极子族的稳定性。对于足够大的雷诺数,内部结构由偶极高宽比a / b(半径与分隔距离)设置,从而产生了一系列光滑的拟稳态解。这些基流解决方案由自蔓延偶极子组成,这些偶极子具有在自适应过程中从偶极子漏出的涡流径迹以及从偶极子开尔文椭圆形上的扩散扩散出来的漏子。目前的工作是对Brion等人最近研究的概括。 (2014年),他发现一种特定类型的涡旋偶极子Lamb-Chaplygin偶极子在二维扰动方面不稳定。我们显示了不稳定模式的增长率和空间结构如何随长宽比a / b和雷诺数变化。生长速率低于Lamb-Chaplygin偶极子的生长速率,而当长宽比降低时则降低。在此提倡,这些新的小长宽比光滑偶极子的二维模式是飞机条件下稳定致动的良好选择。

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