介绍了利用CAD、网格自动剖分和人工智能技术相结合进行航空薄壁结构有限元建模的问题求解框架。
Based on CAD, automatic mesh generation and AI reasoning techniques, the problem solving framework for finite element modeling (FEM) of aeronautical thin wall structures is introduced.
算法将上述非线性问题转化为多个最大流问题求解，并为求解非线性可分凸费用网络流问题提出了通用的求解框架。
This algorithm translates the process of solving NNFPCSC into solving of many maximum flow problems, and provides a general frame for solving NNFPCSC.
最后认为此框架可有效地帮助问题求解中知识表示规范的比较和选择。
It 's believed that this framework can be efficiently used for comparison and selection of knowledge representation scheme in problem solving.
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