Computational simulation and free flight validation of body vibration of flapping-wing MAV in forward flight

2019 ◽  
Vol 95 ◽  
pp. 105491 ◽  
Author(s):  
Dong Xue ◽  
Bifeng Song ◽  
Wenping Song ◽  
Wenqing Yang ◽  
Wenfu Xu ◽  
...  
2021 ◽  
Vol 11 (6) ◽  
pp. 2620
Author(s):  
Yixin Zhang ◽  
Xingjian Wang ◽  
Shaoping Wang ◽  
Wenhao Huang ◽  
Qiwang Weng

To ensure the stability of flight, the butterfly needs to flap its wings and simultaneously move its main body to achieve all kinds of flying motion, such as taking off, hovering, or reverse flight. The high-speed camera is used to record the swing of the abdomen, the movement of the wings, and the pitch angle of the body for butterflies during their free flight; the comprehensive biokinetic observations show that the butterfly’s wings and body are coupled in various flight states. The swing of the abdomen and the flap of the fore wing affect the pitch motion significantly. For theoretical analysis of the butterfly flight, a three-dimensional multi-rigid butterfly model based on real butterfly dimension is established, and the aerodynamic of the butterfly flight is simulated and analyzed via computational fluid dynamics methods to obtain an optimal kinematic model of butterfly forward flight. Moreover, the formation and development of three-dimensional vortex structures in the forward flight are also presented. The detailed structures of vortices and their dynamic behavior show that the wing’s flap and the abdominal swing play a key role in reorienting and correcting the “clap and peel” mechanism, and the force generation mechanisms are evaluated. The research indicates that longitudinal flight performance is mainly related to the kinematic parameters of the wing and body, and it can lead to the development of butterfly-inspired flapping wing air vehicles.


2014 ◽  
Vol 46 (5) ◽  
pp. 055515 ◽  
Author(s):  
Jianyang Zhu ◽  
Chaoying Zhou ◽  
Chao Wang ◽  
Lin Jiang
Keyword(s):  

2019 ◽  
Vol 90 ◽  
pp. 246-263 ◽  
Author(s):  
Ahmed A. Hussein ◽  
Ahmed E. Seleit ◽  
Haithem E. Taha ◽  
Muhammad R. Hajj

AIAA Journal ◽  
2011 ◽  
Vol 49 (8) ◽  
pp. 1750-1762 ◽  
Author(s):  
Hiroto Nagai ◽  
Koji Isogai

Aerospace ◽  
2018 ◽  
Vol 5 (3) ◽  
pp. 83 ◽  
Author(s):  
Hidetoshi Takahashi ◽  
Kosuke Abe ◽  
Tomoyuki Takahata ◽  
Isao Shimoyama

Beetles have attracted attention from researchers due to their unique combination of a passively flapping forewing and an actively flapping hindwing during flight. Because the wing loads of beetles are larger than the wing loads of other insects, the mechanism of beetle flight is potentially useful for modeling a small aircraft with a large weight. In this paper, we present a beetle-type ornithopter in which the wings are geometrically and kinematically modeled after an actual beetle. Furthermore, the forewing is designed to be changeable between no-wing, flapping-wing, or fixed-wing configurations. Micro-electro-mechanical systems (MEMS) differential pressure sensors were attached to both the forewing and the hindwing to evaluate the aerodynamic performance during flight. Whether the forewing is configured as a flapping wing or a fixed wing, it generated constant positive differential pressure during forward flight, whereas the differential pressure on the hindwing varied with the flapping motion during forward flight. The experimental results suggest that beetles utilize the forewing for effective vertical force enhancement.


2017 ◽  
Vol 49 (5) ◽  
pp. 055504
Author(s):  
Kosuke Suzuki ◽  
Takaaki Aoki ◽  
Masato Yoshino

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