Enhancing gust load alleviation performance in an optimized composite wing using passive wingtip devices: Folding and Twist approaches-Reference-Cited by-同舟云学术

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Enhancing gust load alleviation performance in an optimized composite wing using passive wingtip devices: Folding and Twist approaches

Published:2024-04 Issue: Volume:147 Page:109023
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ahmadi Majid,Farsadi Touraj^ORCID,Haddad Khodaparast Hamed^ORCID

Funder

Engineering and Physical Sciences Research Council

TÜBİTAK

Publisher

Elsevier BV

Reference44 articles.

1. Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance;Rajpal;Compos. Struct.,2021

2. Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation;Castrichini;Aeronaut. J.,2017

3. Sizing of high-aspect-ratio wings with folding wingtips;Gu;J. Aircr.,2023

4. Experimental and numerical nonlinear stability analysis of wings incorporating flared folding wingtips;Healy;J. Aircr.,2023

5. Effect of wing stiffness and folding wingtip release threshold on gust loads;Carrillo Córcoles;J. Aircr.,2023

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Optimizing frequencies of functionally graded material plates via multi-objective genetic algorithm: Positioning point supporters for maximum performance;Aerospace Science and Technology;2024-11

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