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The frequency of wing damage in a migrating butterfly

Insect Science 2023年第5期30卷 1507-1517页

作者： Rabiya Korkmaz Hamed Rajabi Shahab Eshghi Stanislav N.Gorb Thies H.Büscher Department of Functional Morphology and Biomechanics Zoological InstituteKiel UniversityKielGermany Division of Mechanical Engineering and Design School of EngineeringLondon South Bank UniversityLondonUK

The ability to fly is crucial for migratory ***,the accumulation of damage on the wings over time can affect survival,especially for species that travel long *** examined the frequency of irreversible wing damage in the migratory butterfly Vanessa cardui to explore the effect of wing structure on wing damage frequency,as well as the mechanisms that might mitigate wing *** exceptionally high migration rate driven by high precipitation levels in their larval habitats in the winter of 2018–2019 provided us with an excellent opportunity to collect data on the frequency of naturally occurring wing damage associated with long-distance *** images of 135 individuals of *** were collected and analyzed in *** results show that the hindwings experienced a greater frequency of damage than the ***,forewings experienced more severe damage on the lateral margin,whereas hindwings experienced more damage on the trailing *** frequency of wing margin damage was higher in the painted lady butterfly than in the migrating monarch butterfly and in the butterfly Pontia occidentalis following artificially induced wing *** results of this study could be used in future comparative studies of patterns of wing damage in butterflies and other *** studies are needed to clarify whether the strategies for coping with wing damage differ between migratory and nonmigratory species.

关键词： biomechanics cost of migration flight Lepidoptera Vanessa cardui wing structure

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基于模型管理框架的机翼结构多目标优化设计(英文)

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Chinese Journal of Aeronautics 2006年第1期19卷 31-35页

作者：安伟刚李为吉苟仲秋 School of Aeronautics Northwestern Polytechnical UniversityXi'an 710072China

Evolutionary algorithm is time-consuming because of the large number of evolutions and much times of finite element analysis, when it is used to optimize the wing structure of a certain high altitude long endurance unmanned aviation vehicle（UAV）. In order to improve efficiency it is proposed to construct a model management framework to perform the multi-objective optimization design of wing structure. The sufficient accurate approximation models of objective and constraint functions in the wing structure optimization model are built when using the model management framework, therefore in the evolutionary algorithm a number of finite element analyses can he avoided and the satisfactory multi-objective optimization results of the wing structure of the high altitude long endurance UAV are obtained.

关键词： wing structure UAV multi-objective opti-mization model management framework SM- MOPSO

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An experimental study of elastic properties of dragonfly-like flapping wings for use in biomimetic micro air vehicles(BMAVs)

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Chinese Journal of Aeronautics 2017年第2期30卷 726-737页

作者： Praveena Nair Sivasankaran Thomas Arthur Ward Erfan Salami Rubentheren Viyapuri Christopher J.Fearday Mohd Rafie Johan Department of Mechanical Engineering University of Malaya KuaIa Lumpur 50603 Malaysia School of Engineering and Physical Sciences Heriot-Watt University Malaysia Putrajaya 62200 Malaysia Department of Electrical Engineering University of Malaya Kuala Lumpur 50603 Malaysia

This article studies the elastic properties of several biomimetic micro air vehicle（BMAV）wings that are based on a dragonfly *** are a new class of unmanned micro-sized air vehicles that mimic the flapping wing motion of flying biological organisms（e.g.,insects,birds,and bats）.Three structurally identical wings were fabricated using different materials：acrylonitrile butadiene styrene（ABS）,polylactic acid（PLA）,and *** wing frame structures were fabricated from these materials and then a nanocomposite film was adhered to them which mimics the membrane of an actual *** wings were then attached to an electromagnetic actuator and passively flapped at frequencies of 10-250 Hz.A three-dimensional high frame rate imaging system was used to capture the flapping motions of these wings at a resolution of 320 pixels x 240 pixels and 35000 frames per *** maximum bending angle,maximum wing tip deflection,maximum wing tip twist angle,and wing tip twist speed of each wing were measured and compared to each other and the actual dragonfly *** results show that the ABS wing has considerable flexibility in the chordwise direction,whereas the PLA and acrylic wings show better conformity to an actual dragonfly wing in the spanwise *** studies have shown that the aerodynamic performance of a BMAV flapping wing is enhanced if its chordwise flexibility is increased and its spanwise flexibility is ***,the ABS wing（fabricated using a 3D printer） shows the most promising results for future applications.

关键词： ABS Acrylic Biomimetic micro air vehicle Flapping mechanism PLA wing structure

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Static strength analysis of dragonfly inspired wings for biomimetic micro aerial vehicles

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Chinese Journal of Aeronautics 2016年第2期29卷 411-423页

作者： Praveena Nair Sivasankaran Thomas Arthur Ward Rubentheren Viyapuri Mohd Rafie Johan Department of Mechanical Engineering University of Malaya

This article examines the suitability of fabricating artificial, dragonfly-like, wing frames from materials that are commonly used in unmanned aircraft （balsa wood, black graphite carbon fiber and red prepreg fiberglass）. wing frames made with Type 321 stainless steel are also examined for comparison. The purpose of these wings is for future use in biomimetic micro aerial vehicles （BMAV）. BMAV are a new class of unmanned micro-sized aerial vehicles that mimic flying biolog- ical organisms （like flying insects）. Insects, such as dragonflies, possess corrugated and complex vein structures that are difficult to mimic. Simplified dragonfly-like wing frames were fabricated from these materials and then a nano-composite film was adhered to them, which mimics the membrane of an actual dragonfly. Finite element analysis simulations were also performed and compared to experimental results. The results showed good agreement （less than 10% difference for all cases）. Analysis of these results shows that stainless steel is a poor choice for this wing configuration, pri- marily because of the aggressive oxidation observed. Steel, as well as balsa wood, also lacks flexi- bility. In comparison, black graphite carbon fiber and red prepreg fiberglass offer some structural advantages, making them more suitable for consideration in future BMAV applications.

关键词： Biomimetic micro aerialvehicle Carbon fiber Finite element analysis Glass fiber wing membrane wing structure

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