Flutter prediction of composite wing using finite element method with equivalent stiffness

被引：0
|
作者：
Ouyang, Xing [1 ]
Yu, Xiong-Qing [1 ]
Wang, Yu [1 ]
机构：
[1] Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源：
Zhendong Gongcheng Xuebao/Journal of Vibration Engineering | 2015年 / 28卷 / 03期
关键词：
Aircraft preliminary design - Equivalent stiffness - Flutter analysis - Model and analysis - Preliminary design - Stiffness matrices - Stringer-stiffened panels - Structural layout;
D O I：
10.16385/j.cnki.issn.1004-4523.2015.03.009
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：404 / 410
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