Experimental Structural Design of a Novel Variable-Sweep Wing Based on a Four-Bar Planar Linkage-Reference-Cited by-同舟云学术

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Experimental Structural Design of a Novel Variable-Sweep Wing Based on a Four-Bar Planar Linkage

Published:2024-11 Issue:6 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cheng Gui¹,Song Keyao²^ORCID,Jiang Tianjian¹,Yang Jun³,Zhou Xiang⁴^ORCID

Affiliation:

1. Ph.D. Candidate, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., Shanghai 200240, China.

2. Postdoc, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., Shanghai 200240, China. ORCID: .

3. Chengdu Aircraft Design and Research Institute, Chengdu 610091, China.

4. Associate Professor, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., Shanghai 200240, China (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5708

Reference52 articles.

1. Recent developments in the aeroelasticity of morphing aircraft

2. Morphing wings review: aims, challenges, and current open issues of a technology

3. Aircraft Morphing—An Industry Vision

4. Investigation of Smart Material Actuators & Aerodynamic optimization of Morphing Wing

5. Design prototyping methods: state of the art in strategies, techniques, and guidelines

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