Design and Analysis of a Morphing Trailing Edge Structure

被引：0
|
作者：
Wang, Z. [1 ]
Yang, Y. [1 ]
Duan, S. [1 ]
Sun, X. [2 ]
机构：
[1] Aircraft Strength Res Inst, Xian 710065, Peoples R China
[2] Chinese Aeronaut Estab, Beijing 100012, Peoples R China
来源：
ICCM 21: 21ST INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS (ICCM-21) | 2017年
关键词：
morphing wing; trailing edge; compliant structures; topology optimization;
D O I：
暂无
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
The need for a next generation of air vehicles that has high performance and low environmental impact has gained during the past years due to the "green-liner" demands on civil aeronautics
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收藏
页数：4
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