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- W2316874539 abstract "Research on insect flight has been propelled by the growing interest in Micro Air Vehicles (MAVs). Typical flapping wing MAVs fly in the low Reynolds number regime of 10 3 -10 4 , similar to that of insects. A critical review on the progress of research on the effects of aerodynamics/kinematics and aeroelasticity on flapping wing propulsion reveals the complexity of the subject. Multiple factors are intertwined and influence the propulsion and aerodynamic performance of a wing/insect, thus necessitating the study of a variety of insects and flapping techniques. Bumblebees are chosen as a case study due to their desirable characteristics for MAV applications. The purpose of this paper is to provide a numerical analysis of the propulsion of bumblebees. A numerical study is conducted to investigate the effects of wing-body interactions and flexibility on bumblebee propulsion. Firstly the insect wings and body are modelled as rigid bodies. Three computational models are created with only the wing-pair, the wing-pair with narrower gap between the wings, and both the wings and the body. The numerical results of the rigid model agree well with the experimental measurement, with a vortex-ring pattern observed during the downstroke. Comparison of the three computational models suggests that the vortex pattern does not result from having a wide thorax, where the wing-pair is separated by a large gap. The two-way FSI flexible bumblebee wing simulations show that flexible wings produce higher time-averaged lift and thrust than the rigid wing." @default.
- W2316874539 created "2016-06-24" @default.
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- W2316874539 date "2013-06-22" @default.
- W2316874539 modified "2023-09-22" @default.
- W2316874539 title "A Numerical Analysis of Bumblebee Propulsion" @default.
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- W2316874539 doi "https://doi.org/10.2514/6.2013-3049" @default.
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