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Insect wings and biomimetic wings in flapping-wing micro air vehicles (FWMAVs) are flexible and subject to passive deformations, including spanwise twisting and bending. This raises a typical bilateral fluid–structure interaction (FSI) issue, which is conventionally solved based on combined computational fluid dynamics (CFD) and computational solid dynamics (CSD) methods. To reduce the computational cost of this FSI issue while maintaining a reasonable accuracy, a theoretical model with improved adaptability is proposed here. The improvement results from the consideration of spanwise bending: the distribution of which is formulated by a quadratic polynomial. The aerodynamic force is approximated by a predictive quasi-steady aerodynamic model based on the blade element theory. The FSI iteration at a time step is converged within 0.5s in our model, whereas a traditional CFD–CSD solution takes about 30s. Compared to our previous model, the current model can better match the experimental measurements of insect wings. Further analysis reveals that considering spanwise bending affects the stiffness design of flexible flapping wings quantitatively. To maintain a high lift efficiency, the structural stiffness of the wing should be appropriately decreased. Our model provides a refined tool for the wing design in FWMAVs and can promote the development of FWMAVs. Abstract
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Most cited references40
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Wing rotation and the aerodynamic basis of insect flight.
M Dickinson, F. -O. Lehmann, S P Sane (1999)
The enhanced aerodynamic performance of insects results from an interaction of three distinct yet interactive mechanisms: delayed stall, rotational circulation, and wake capture. Delayed stall functions during the translational portions of the stroke, when the wings sweep through the air with a large angle of attack. In contrast, rotational circulation and wake capture generate aerodynamic forces during stroke reversals, when the wings rapidly rotate and change direction. In addition to contributing to the lift required to keep an insect aloft, these two rotational mechanisms provide a potent means by which the animal can modulate the direction and magnitude of flight forces during steering maneuvers. A comprehensive theory incorporating both translational and rotational mechanisms may explain the diverse patterns of wing motion displayed by different species of insects.
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Flexural stiffness in insect wings. I. Scaling and the influence of wing venation.
S Combes, Roy Daniel (2003)
During flight, many insect wings undergo dramatic deformations that are controlled largely by the architecture of the wing. The pattern of supporting veins in wings varies widely among insect orders and families, but the functional significance of phylogenetic trends in wing venation remains unknown, and measurements of the mechanical properties of wings are rare. In this study, we address the relationship between venation pattern and wing flexibility by measuring the flexural stiffness of wings (in both the spanwise and chordwise directions) and quantifying wing venation in 16 insect species from six orders. These measurements show that spanwise flexural stiffness scales strongly with the cube of wing span, whereas chordwise flexural stiffness scales with the square of chord length. Wing size accounts for over 95% of the variability in measured flexural stiffness; the residuals of this relationship are small and uncorrelated with standardized independent contrasts of wing venation characters. In all species tested, spanwise flexural stiffness is 1-2 orders of magnitude larger than chordwise flexural stiffness. A finite element model of an insect wing demonstrates that leading edge veins are crucial in generating this spanwise-chordwise anisotropy.
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Details of insect wing design and deformation enhance aerodynamic function and flight efficiency.
Adam Walker, Richard Bomphrey, Adrian L R Thomas … (2009)
Insect wings are complex structures that deform dramatically in flight. We analyzed the aerodynamic consequences of wing deformation in locusts using a three-dimensional computational fluid dynamics simulation based on detailed wing kinematics. We validated the simulation against smoke visualizations and digital particle image velocimetry on real locusts. We then used the validated model to explore the effects of wing topography and deformation, first by removing camber while keeping the same time-varying twist distribution, and second by removing camber and spanwise twist. The full-fidelity model achieved greater power economy than the uncambered model, which performed better than the untwisted model, showing that the details of insect wing topography and deformation are important aerodynamically. Such details are likely to be important in engineering applications of flapping flight.
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Author and article information
Contributors
Feng Liu Yang
Long Chen:
ORCID: https://orcid.org/0000-0002-0222-2665
Yan Qing Wang
Journal
Journal ID (publisher-id): aiaaj
Title: AIAA Journal
Abbreviated Title: AIAA Journal
Publisher: American Institute of Aeronautics and Astronautics
ISSN (Electronic): 1533-385X
Publication date (Electronic): 29 August 2022
Publication date (Print): December 2022
Volume: 60
Issue: 12
Pages: 6680-6691
Affiliations
Author notes
[†]
Assistant Professor, Key Laboratory of Structural Dynamics of Liaoning Province, College of Sciences.
[‡]
Professor, Key Laboratory of Structural Dynamics of Liaoning Province, College of Sciences; Key Laboratory of Ministry of Education on Safe Mining of Deep Metal Mines; wangyanqing@ 123456mail.neu.edu.cn (Corresponding Author).
Author information
Long Chen https://orcid.org/0000-0002-0222-2665
Article
Publisher ID: J061726 Manuscript ID: J061726
DOI: 10.2514/1.J061726
SO-VID: 890f9571-f139-4f94-9106-1770ebb24113
Copyright © Copyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
History
Date received : 10 February 2022
Date revision received : 13 July 2022
Date accepted : 16 July 2022
Page count
Figures: 11, Tables: 1
Funding
Funded by: Department of Science and Technology of Liaoning Provincehttp://dx.doi.org/10.13039/501100012131
Award ID: 2021-BS-057
Funded by: Fundamental Research Funds for the Central Universities
Award ID: N2005019
Funded by: National Natural Science Foundation of Chinahttp://dx.doi.org/10.13039/501100001809
Award ID: 11922205
Award ID: 12002082
Categories
Subject: Regular Articles
ScienceOpen disciplines: Engineering,Physics,Mechanical engineering,Space Physics
Data availability:
ScienceOpen disciplines: Engineering, Physics, Mechanical engineering, Space Physics
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Most referenced authors206
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