Equations of motion for weakly compressible point vortices

Stefan G. Llewellyn Smith, T. Chu, Z. Hu
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引用次数: 2

Abstract

Equations of motion for compressible point vortices in the plane are obtained in the limit of small Mach number, M, using a Rayleigh–Jansen expansion and the method of Matched Asymptotic Expansions. The solution in the region between vortices is matched to solutions around each vortex core. The motion of the vortices is modified over long time scales O(M2log⁡M) and O(M2). Examples are given for co-rotating and co-propagating vortex pairs. The former show a correction to the rotation rate and, in general, to the centre and radius of rotation, while the latter recover the known result that the steady propagation velocity is unchanged. For unsteady configurations, the vortex solution matches to a far field in which acoustic waves are radiated. This article is part of the theme issue ‘Mathematical problems in physical fluid dynamics (part 2)’.
弱可压缩点涡的运动方程
利用Rayleigh-Jansen展开法和匹配渐近展开法,得到了平面上可压缩点涡在小马赫数M极限下的运动方程。涡旋之间区域的解与每个涡旋核心周围的解相匹配。涡旋的运动在长时间尺度O(M2log (M)和O(M2)上得到修正。给出了共旋转和共传播涡旋对的例子。前者显示了对旋转速率的修正,一般来说,对旋转中心和半径的修正,而后者恢复了已知的稳态传播速度不变的结果。对于非定常结构,涡旋解与声波辐射的远场相匹配。本文是主题问题“物理流体动力学中的数学问题(第二部分)”的一部分。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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