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Nonstationary westward translation of nonlinear frontal warm-core eddies

机译:非线性额热核涡的非平稳西移

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摘要

For the first time, an analytical theory and a very high-resolution, frontal numerical model, both based on the unsteady, nonlinear, reduced-gravity shallow water equations on a beta plane, have been used to investigate aspects of the migration of homogeneous surface, frontal warm-core eddies on a beta plane. Under the assumption that, initially, such vortices are surface circular anticyclones of paraboloidal shape and having both radial and azimuthal velocities that are linearly dependent on the radial coordinate (i.e., circular pulsons of the first order), approximate analytical expressions are found that describe the nonstationary trajectories of their centers of mass for an initial stage as well as for a mature stage of their westward migration. In particular, near-inertial oscillations are evident in the initial migration stage, whose amplitude linearly increases with time, as a result of the unbalanced vortex initial state on a beta plane. Such an initial amplification of the vortex oscillations is actually found in the first stage of the evolution of warm-core frontal eddies simulated numerically by means of a frontal numerical model initialized using the shape and velocity fields of circular pulsons of the first order. In the numerical simulations, this stage is followed by an adjusted, complex nonstationary state characterized by a noticeable asymmetry in the meridional component of the vortex's horizontal pressure gradient, which develops to compensate for the variations of the Coriolis parameter with latitude. Accordingly, the location of the simulated vortex's maximum depth is always found poleward of the location of the simulated vortex's center of mass. Moreover, during the adjusted stage, near-inertial oscillations emerge that largely deviate from the exactly inertial ones characterizing analytical circular pulsons: a superinertial and a subinertial oscillation in fact appear, and their frequency difference is found to be an increasing function of latitude. A comparison between vortex westward drifts simulated numerically at different latitudes for different vortex radii and pulsation strengths and the corresponding drifts obtained using existing formulas shows that, initially, the simulated vortex drifts correspond to the fastest predicted ones in many realistic cases. As time elapses, however, the development of a beta-adjusted vortex structure, together with the effects of numerical dissipation, tend to slow down the simulated vortex drift.
机译:第一次,基于贝塔平面上的非稳态,非线性,低重力浅水方程组的分析理论和非常高分辨率的正面数值模型,已用于研究均质表面迁移的各个方面,在beta飞机上的正面暖核涡流。假设这些旋涡最初是抛物面形的表面圆形反旋风,并且径向和方位角速度都线性依赖于径向坐标(即一阶圆形脉冲),则可以找到近似解析表达式来描述他们的质心向西迁移的初始阶段和成熟阶段的非平稳轨迹。特别是,在初始迁移阶段,近惯性振荡是显而易见的,由于β平面上涡流初始状态不平衡,其振幅随时间线性增加。涡流振荡的这种初始放大实际上是在通过使用一阶圆形脉冲子的形状和速度场初始化的额叶数值模型通过数值模拟的暖芯额叶涡流演化的第一阶段中发现的。在数值模拟中,此阶段之后是经过调整的复杂非平稳状态,其特征是涡旋水平压力梯度的子午分量明显不对称,从而发展以补偿科里奥利参数随纬度的变化。因此,总会发现模拟涡旋的最大深度的位置在模拟涡旋的质心的位置的最前方。此外,在调整阶段,出现了接近惯性的振动,该振动与表征分析圆形脉冲的精确惯性有很大不同:实际上出现了惯性和次惯性振动,并且发现它们的频率差是纬度的增加函数。在不同纬度上针对不同涡旋半径和脉动强度进行数值模拟的涡旋向西漂移与使用现有公式获得的相应漂移之间的比较表明,在许多实际情况下,模拟的涡流漂移最初对应于最快的预测漂移。但是,随着时间的流逝,经过β调整的涡旋结构的发展以及数值耗散的影响,往往会减慢模拟的涡旋漂移。

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