In the paper the phenomena in test for nonlinear dynamic behavior of aluminum honeycomb sandwich plate in satellite structure are analysed.
本文针对卫星主要结构材料铝质蜂窝板的非线性动力特性现象进行了振动试验及分析。
Rules of these linear or nonlinear and dynamic phenomena were unveiled using graph.
并以图形化方式揭示了这些动态的、线性或非线性现象的规律。
The necessary condition of presenting bifurcation and chaos phenomena in dynamic systems is that the systems are nonlinear ones.
动力学系统中分岔与混沌现象产生的必要条件之一，就是该系统必须是非线性的。
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