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- W3139820095 abstract "因为有限元素分析预处理的费时间的特征，飞机翅膀的参量的建模方法组织的一个有限元素在这份报纸被建议。主要研究在飞机结构的初步的设计阶段期间被放。快有限元素建模的一个知识驱动的系统被造。基于这个方法，采用一个模板参量的技术，包括设计方法的知识，规则，和在当模特儿的进程的专家经验被包含，一个有限元素模型自动地被建立，它极大地改进速度，精确性，和标准化当模特儿的度。骨骼模型，几何网孔模型，和包括有限元素网孔和性质数据的有限元素模型在参量的描述和自动更改上被建立。研究的结果证明方法在为参量的分析和优化设计的有限元素建立一个关键技术基础的有限元素建模的过程解决参数协会和模型更改的一系列问题。" @default.
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- W3139820095 date "2013-01-01" @default.
- W3139820095 modified "2023-09-24" @default.
- W3139820095 title "A finite element parametric modeling technique of aircraft wing structures" @default.
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