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Design and testing of a full-scale variable-camber leading edge based on a composite compliant skin and an open-kinematic-chain mechanism

Zhigang WANG Xiasheng SUN Yu YANG Jin ZHOU Chunpeng LI Daochun LI Jinwu XIANG

中国航空学报（英文版）2025，Vol.38Issue(12)：245-262,18.

中国航空学报（英文版）2025，Vol.38Issue(12)：245-262,18.DOI:10.1016/j.cja.2025.103714

Design and testing of a full-scale variable-camber leading edge based on a composite compliant skin and an open-kinematic-chain mechanism

Zhigang WANG ¹Xiasheng SUN ²Yu YANG ³Jin ZHOU ⁴Chunpeng LI ⁵Daochun LI ⁶Jinwu XIANG⁶

作者信息

1. School of Aeronautical Science and Engineering,Beihang University,Beijing 100191,China||National Key Laboratory of Strength and Structural Integrity,Aircraft Strength Research Institute of China,Xi'an 710065,China
2. School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China
3. National Key Laboratory of Strength and Structural Integrity,Aircraft Strength Research Institute of China,Xi'an 710065,China
4. Chinese Aeronautical Establishment,Beijing 100012,China
5. Aviation Key Laboratory of Science and Technology on High Speed and High Reynolds Number Aerodynamic Force Research,AVIC Aerodynamics Research Institute,Shenyang 110034,China
6. School of Aeronautical Science and Engineering,Beihang University,Beijing 100191,China
折叠

摘要

关键词

Compliant skin/Intelligent structures/Morphing leading edge/Optimization/Smart droop nose

Key words

Compliant skin/Intelligent structures/Morphing leading edge/Optimization/Smart droop nose

引用本文复制引用

Zhigang WANG,Xiasheng SUN,Yu YANG,Jin ZHOU,Chunpeng LI,Daochun LI,Jinwu XIANG..Design and testing of a full-scale variable-camber leading edge based on a composite compliant skin and an open-kinematic-chain mechanism[J].中国航空学报（英文版）,2025,38(12):245-262,18.

基金项目

This work was supported by the National Research Project"Variable CAmber wing TechNology(VCAN)",China. （VCAN）

中国航空学报（英文版）

ISSN：1000-9361

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