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定常对称背涡流态下细长体绕流结构的演变 被引量:3

Structure evolution of the steady and symmetric vortex pattern around a slender
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摘要 应用数值计算的方法模拟了细长体截面绕流结构的演变过程 .指出随着细长体背涡的发展 ,导致截面流场的拓扑结构发生变化 ,会出现一种临界流动状态 .并用微分方程的定性理论分析了此时流场中出现的一种高阶奇点 .这种高阶奇点的指数为 - 3 2 ,它是结构不稳定的 ,稍有扰动就会产生分叉 ,使流场的拓扑结构发生变化 .得出了定常对称背涡流态下细长体的空间绕流结构图 . The structure evolution of flow pattern around a slender was calculated by numerical method. It was pointed that the development of slender vortices leads to the change of topological structure about cross flow, and a critical flow pattern will appear. A high-order singular point in this flow field was analysed by differential equation qualitative theory. The index of the high-order singular is -3/2. The topological structure of this singular point is instable, so bifurcation will be occurred and the topological structure of flow field will be changed by little disturbance. The 3-dimensional flow structure of the steady and symmetric vortices pattern around a slender was gained.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2005年第2期167-171,共5页 Journal of Beijing University of Aeronautics and Astronautics
基金 国家自然科学基金资助项目 (10 172 0 17) 航空基础科学基金资助项目 (0 2A5 10 48)
关键词 细长体 拓扑 高阶奇点 分叉 结构稳定性 Bifurcation (mathematics) Computer simulation Differential equations Flow patterns Numerical methods Stability Structures (built objects) Topology
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参考文献1

  • 1Lowson M V, Ponton A J.Symmetry breaking in vortex flows on conical bodies [J].AIAA Journal, 1995,30(6):1576~1583.

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