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首页> 外文期刊>Journal of Fluid Mechanics >Analogies and differences between the stability of an isolated pancake vortex and a columnar vortex in stratified fluid
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Analogies and differences between the stability of an isolated pancake vortex and a columnar vortex in stratified fluid

机译:分层流体中分离的煎饼旋涡和圆柱旋涡的稳定性之间的类比和差异

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In order to understand the dynamics of pancake shaped vortices in stably stratified fluids, we perform a linear stability analysis of an axisymmetric vortex with Gaussian angular velocity in both the radial and axial directions with an aspect ratio of alpha. The results are compared to those for a columnar vortex (alpha = infinity) in order to identify the instabilities. Centrifugal instability occurs when R > c(m) where R = ReFh2 is the buoyancy Reynolds number, F-h the Froude number, Re the Reynolds number and c(m) a constant which differs for the three unstable azimuthal wavenumbers m = 0, 1, 2. The maximum growth rate depends mostly on R and is almost independent of the aspect ratio alpha. For sufficiently large buoyancy Reynolds number, the axisymmetric mode is the most unstable centrifugal mode whereas for moderate R, the mode m = 1 is the most unstable. Shear instability for m = 2 develops only when F-h <= 0.5 alpha. By considering the characteristics of shear instability for a columnar vortex with the same parameters, this condition is shown to be such that the vortex is taller than the minimum wavelength of shear instability in the columnar case. For larger Froude number F-h >= 1.5 alpha, the isopycnals overturn and gravitational instability can operate. Just below this threshold, the azimuthal wavenumbers m = 1, 2, 3 are unstable to baroclinic instability. A simple model shows that baroclinic instability develops only above a critical vertical Froude number F-h/alpha because of confinement effects.
机译:为了了解稳定分层流体中薄饼形涡旋的动力学特性,我们对轴对称涡旋进行了线性稳定性分析,该轴对称涡旋在径向和轴向均具有高斯角速度,且纵横比为α。将结果与圆柱状涡旋(α=无穷大)的结果进行比较,以确定不稳定性。当R> c(m)时会发生离心不稳定性,其中R = ReFh2是浮力雷诺数,Fh是Froude数,Re雷诺数和c(m)是一个常数,对于三个不稳定的方位波数m = 0、1, 2.最大增长率主要取决于R,并且几乎与纵横比alpha无关。对于足够大的浮力雷诺数,轴对​​称模式是最不稳定的离心模式,而对于中等R,模式m = 1是最不稳定的。仅当F-h <= 0.5 alpha时,才会出现m = 2的剪切不稳定性。通过考虑具有相同参数的柱状涡旋的剪切不稳定性的特性,表明该条件使得该涡旋比柱状情况下的剪切不稳定性的最小波长高。对于更大的弗劳德数F-h> = 1.5 alpha,可以等位面倾覆和重力不稳定。刚好低于此阈值,方位波数m = 1、2、3对于斜压不稳定是不稳定的。一个简单的模型表明,由于限制效应,斜压不稳定仅在临界弗洛德数F-h / alpha之上出现。

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