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Design and experimental verification of a large-scale coupled morphing-wing mechanism for hypersonic vehicles

Yanbing Wang Honghao Yue Xueting Pan Jun Wu Fei Yang Yong Zhao Xue Bai Jicheng Liu

Defence Technology(防务技术)2026，Vol.56Issue(2)：P.125-141,17.

Defence Technology(防务技术)2026，Vol.56Issue(2)：P.125-141,17.DOI:10.1016/j.dt.2025.10.031

Design and experimental verification of a large-scale coupled morphing-wing mechanism for hypersonic vehicles

Yanbing Wang ¹Honghao Yue ¹Xueting Pan ¹Jun Wu ¹Fei Yang ¹Yong Zhao ¹Xue Bai ²Jicheng Liu²

作者信息

1. School of Mechatronics Engineering,Harbin Institute of Technology,Harbin,150001,China
2. Beijing Institute of Electronic System Engineering,Beijing,100854,China
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摘要

关键词

Hypersonic vehicle/Coupled morphing wing/Locking/release/Active stiffness control/Distributed loading

分类

航空航天

引用本文复制引用

Yanbing Wang,Honghao Yue,Xueting Pan,Jun Wu,Fei Yang,Yong Zhao,Xue Bai,Jicheng Liu..Design and experimental verification of a large-scale coupled morphing-wing mechanism for hypersonic vehicles[J].Defence Technology(防务技术),2026,56(2):P.125-141,17.

基金项目

supported by the National Natural Science Foundation of China(Grant No.52405257) （Grant No.52405257）

the China Postdoctoral Science Foundation(Grant No.2024M764201). （Grant No.2024M764201）

Defence Technology(防务技术)

ISSN：2096-3459

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