摘要
为解决翼面结构参数化设计的问题,研究了翼面结构各组成元件的个数、位置、截面尺寸参数化描述的方法。基于这些参数研究如何通过CATIA二次开发方式自动生成翼面结构三维图以及从总体模型获取机翼外形参数。在对翼面结构参数化描述的基础上,应用Visual Studio环境下CATIA二次开发技术,结合VB和C++语言混合编程,实现翼面结构的参数化设计。
In order to solve the problem of the wing structure parametric design, based on the study of parameters described method that the number of the various components of the wing structure, location, the cross-sectional size, on how to automatically generate wing structure three-dimensional shape by CATIA secondary development, and to obtain wing surface parameters of the aircraft model are studied. The application of CATIA secondary development technology in the Visual Studio environment on the basis of the description of the structural parameters of the wing structure, combined with the VB and C＋＋ languages mixed programming, parametric design of the wing structure is realized.
出处
《计算机工程与设计》
CSCD
北大核心
2013年第7期2580-2584,共5页
Computer Engineering and Design
