The design of modern carbon-based beam-like aircraft and spacecraft panels is complex and cost-consuming from an experimental point of view. Effective computational approaches to vibration problems of these structures are expected and desired to create numerical tools for their optimization and analysis, especially in the nonlinear regime of problems.

中文翻译：

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纳米复合梁状航空航天结构的非线性动力学


从实验的角度来看，现代碳基梁状飞机和航天器面板的设计非常复杂且成本高昂。人们期望并期望对这些结构的振动问题进行有效的计算方法来创建用于优化和分析的数值工具，特别是在问题的非线性领域。