Finite Element Method Based Modeling of a Flexible Wing Structure

被引：0
|
作者：
Svoboda, Filip [1 ]
Hromcik, Martin [1 ]
机构：
[1] Czech Tech Univ Praque, Fac Elect Engn, Karlovo Namest 13-E, Prague 12135, Czech Republic
来源：
2017 21ST INTERNATIONAL CONFERENCE ON PROCESS CONTROL (PC) | 2017年
关键词：
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The finite element based structural model of a flexible wing is presented. The structural model will be a part of a servoelastic wing used for flutter analysis and designing flutter suppression control systems. It also allows modal analysis of a wing with given parameters. A finite element model consists of Euler-Bernoulli beams joined together. This approach is able to reach high accuracy and various properties of a particular wing element can be modeled.
引用
收藏
页码：222 / 227
页数：6
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