航空科学技术Issue(9)：23-28,6.
基于可行方向法的机翼盒段结构参数优化设计
The Wing Box Structure Parameter Optimization Design Based on MFD
王晓阳 1姚雄华1
作者信息
- 1. 中航工业第一飞机设计研究院，陕西 西安 710089
- 折叠
摘要
Abstract
Using TCL language to redevelop the HyperWorks, established the local stability response of stringer and skin area ratio the upper skin and the beam web and associated component geometry parameters. The paper proposed a smal step iteration hierarchical optimization based on MFD, and optimized a wing box structure of a civil aircraft by using this method and realized the weight reduction of the wing box structure.关键词
机翼/盒段结构/参数优化/可行方向法/稳定性/TCL语言Key words
wing/box structure/parameter optimization/MFD/stability/TCL language分类
航空航天引用本文复制引用
王晓阳,姚雄华..基于可行方向法的机翼盒段结构参数优化设计[J].航空科学技术,2015,(9):23-28,6.
