Design optimization and testing of a morphing leading-edge with a variable-thickness compliant skin and a closed-chain mechanism-Reference-Cited by-同舟云学术

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Design optimization and testing of a morphing leading-edge with a variable-thickness compliant skin and a closed-chain mechanism

Published:2024-07 Issue:7 Volume:37 Page:285-300
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

WANG Zhigang^ORCID,SUN Xiasheng,YANG Yu,GE Wenjie,LI Daochun,XIANG Jinwu,BAO Panpan,WU Qi,DA RONCH Andrea

Publisher

Elsevier BV

Reference48 articles.

1. Air Transport Action Group [Internet]. Geneva: Air Transport Action Group; [cited 2023 Oct 17]. Available from: https://aviationbenefits.org/environmental-efficiency/climate-action/waypoint-2050/.

2. International Civil Aviation Organization [Internet]. Montreal: International Civil Aviation Organization; [cited 2023 Oct 17]. Available from: https://www.icao.int/environmental-protection/Pages/envrep2022.aspx.

3. Bolonkin A, Gilyard G. Estimated benefits of variable-geometry wing camber control for transport aircraft. Washington, D.C.: National Technical Information Service (NTIS); 1999. Report No.: NASA/TM-1999-206586.

4. Multifunctional wing moveables: Design of the A350XWB and the way to future concepts;Reckzeh,2014

5. The aerodynamic design of the A350 XWB-900 high lift system;Strüber,2014

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