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间隙约束二元翼段系统分岔与多解共存现象分析

尹磊磊 张思进 文桂林 徐慧东

尹磊磊, 张思进, 文桂林, 徐慧东. 间隙约束二元翼段系统分岔与多解共存现象分析[J]. 航空动力学报, 2014, (6): 1410-1416. doi: 10.13224/j.cnki.jasp.2014.06.022
引用本文: 尹磊磊, 张思进, 文桂林, 徐慧东. 间隙约束二元翼段系统分岔与多解共存现象分析[J]. 航空动力学报, 2014, (6): 1410-1416. doi: 10.13224/j.cnki.jasp.2014.06.022
YIN Lei-lei, ZHANG Si-jin, WEN Gui-lin, XU Hui-dong. Analysis on the system bifurcation and coexistence of multiple solutions for typical airfoil section with freeplay[J]. Journal of Aerospace Power, 2014, (6): 1410-1416. doi: 10.13224/j.cnki.jasp.2014.06.022
Citation: YIN Lei-lei, ZHANG Si-jin, WEN Gui-lin, XU Hui-dong. Analysis on the system bifurcation and coexistence of multiple solutions for typical airfoil section with freeplay[J]. Journal of Aerospace Power, 2014, (6): 1410-1416. doi: 10.13224/j.cnki.jasp.2014.06.022

间隙约束二元翼段系统分岔与多解共存现象分析

doi: 10.13224/j.cnki.jasp.2014.06.022
基金项目: 

国家杰出青年科学基金(11225212);国家自然科学基金(11372101,11002052)

详细信息
    作者简介:

    尹磊磊(1989- ),男,湖北汉川人,硕士生,主要从事非光滑动力学研究.

    通讯作者:

    张思进(1971- ),男,安徽潜山人,教授,主要从事非光滑动力学、动力学控制、复合材料动力学及分岔控制理论等方面的研究.

  • 中图分类号: V211.41;V211.3

Analysis on the system bifurcation and coexistence of multiple solutions for typical airfoil section with freeplay

  • 摘要: 研究了分段刚度描述的间隙约束二元翼段气动弹性系统,取俯仰角最大幅值处为类 Poincaré 截面,数值计算得到了系统随飞行速度变化的分岔图,发现飞行速度在Ma=0.71~0.75属于跨临界颤振区,而在Ma=0.75~0.95发生极限环震荡.同时通过构造极限环震荡的四维Poincaré映射分析了极限环震荡的稳定性,结合稳定性和运动流形理论,得到极限环震荡的吸引域一般位于极限环内部并用数值方法进行了验证.且跨临界颤振速度区域中存在多种分岔形式以及多解共存现象,例如由双周期运动直接通向混沌、多周期运动与双周期运动共存现象,振动幅值也存在跳跃现象.

     

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出版历程
  • 收稿日期:  2013-04-08
  • 刊出日期:  2014-06-28

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