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Tearing instability of isolated compressible vortices

机译:分离的可压缩涡流的不稳定性

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The present paper addresses the instability of a compressible vortex flow. We consider a family of so-called isolated vortices - the circular planar vortices that have zero circulation (net vorticity). The term "isolation" implies the presence of a shield in the vorticity field - a region of vorticity of common sign surrounding the central domain where the vorticity is oppositely signed. To model such a vorticity field, a generalized Taylor-type profile for the swirl velocity in the radial direction is employed, which involves two parameters: intensity μ (proportional to the maximal velocity) and steepness β (characterizing the scale of the shield zone). Vortices are assumed to be compressible and homentropic. The linear-stability analysis is carried out, which shows that isolated vortices can exhibit both stable and unstable behavior depending on the model parameters μ and β. By numerical simulations of the non-linear stage, the unstable normal modes are shown to evolve towards tearing of the basic vortex with formation of smaller secondary vortical structures.
机译:本文解决了可压缩涡流的不稳定性。我们考虑一个所谓的孤立涡旋族-循环为零(净涡旋度)的圆形平面涡旋。术语“隔离”表示在涡度场中存在屏蔽层-围绕中心区域的共同符号的涡度区域,在中心区域中涡度被相反地签名。为了模拟这样的涡旋场,采用了径向方向上旋涡速度的广义泰勒型轮廓,它涉及两个参数:强度μ(与最大速度成比例)和陡度β(表征屏蔽区的尺度) 。涡流被认为是可压缩的并且是同质的。进行了线性稳定性分析,结果表明,取决于模型参数μ和β,孤立的涡流可以同时表现出稳定和不稳定的行为。通过非线性阶段的数值模拟,不稳定的法向模态显示出随着形成较小的次级涡旋结构而向基本涡旋的撕裂方向发展。

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