摘要
扩展了圆域中涡旋流动的两层准地转轮廓动力学方法。阐述控制方程模型及其一些基本特性的数值实现。通过拟稳态线性稳定性分析,得出对称潜涡流小于4线的间断潜涡流分布情况。对于非稳定上层屏蔽朗肯旋涡情况的实验结果进行讨论,结果发现,支配扰动波长的变化导致在涡旋底部中心为主的上部旋涡结构中心的初始位移。
To study the vortex flows a two-layer quasi-geostrophic version of the contour-dynamics method was extended in a round domain.Governing equations of the model was setup,and some basic features of the numerical implementation were presented.Linear stability analysis was made for the case of axially symmetric potential vorticity(PV) distributions with less than four lines of PV discontinuity.The case of unsteady upper-layer shielded Rankine vortex was discussed.The results were shown that there was the initial displacement of the center of above vortex structure from the basin center in changes of dominated disturbance wave length.
出处
《沈阳化工大学学报》
CAS
2011年第3期283-288,共6页
Journal of Shenyang University of Chemical Technology
基金
support from the Ministry of Education and Science of Russia(federal program"Development of staff for the science and education"2009~2013,State contract N П1073)
关键词
轮廓动态学
二层准地转模型
朗肯涡
非稳定
contour dynamics
two-layer quasi-geostrophic model
rankine vortex
instability