2021
DOI: 10.1098/rsos.202172
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Beneficial wake-capture effect for forward propulsion with a restrained wing-pitch motion of a butterfly

Abstract: Unlike other insects, a butterfly uses a small amplitude of the wing-pitch motion for flight. From an analysis of the dynamics of real flying butterflies, we show that the restrained amplitude of the wing-pitch motion enhances the wake-capture effect so as to enhance forward propulsion. A numerical simulation refined with experimental data shows that, for a small amplitude of the wing-pitch motion, the shed vortex generated in the downstroke induces air in the wake region to flow towards the wings. This condit… Show more

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Cited by 16 publications
(15 citation statements)
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“…As a result, at the beginning of the experiment, the average aerodynamic lift in one period is 0.044 N, and the motion parameters are (51 • , −14 • , 0.35, 1.7 Hz), the agent finds the appropriate motion parameters that the amplitude, the middle position, the downstroke ratio and the flapping frequency are (73 • , −12 • , 0.3, 2 Hz), respectively. The flapping amplitude is evidently different from the real butterfly [30]. Under this setting, the average aerodynamic lift in one period reaches 0.861 N and the lift force curves in figure 6 show that a conventional lift peak is generated in the downstroke stage, but an unexpected strong lift peak is generated in the upstroke stage.…”
Section: Resultsmentioning
confidence: 85%
“…As a result, at the beginning of the experiment, the average aerodynamic lift in one period is 0.044 N, and the motion parameters are (51 • , −14 • , 0.35, 1.7 Hz), the agent finds the appropriate motion parameters that the amplitude, the middle position, the downstroke ratio and the flapping frequency are (73 • , −12 • , 0.3, 2 Hz), respectively. The flapping amplitude is evidently different from the real butterfly [30]. Under this setting, the average aerodynamic lift in one period reaches 0.861 N and the lift force curves in figure 6 show that a conventional lift peak is generated in the downstroke stage, but an unexpected strong lift peak is generated in the upstroke stage.…”
Section: Resultsmentioning
confidence: 85%
“…While some studies (e.g., Zheng et al, 2013;Johansson and Henningsson, 2020) suggested the importance of wing deformation in terms of aerodynamic performance, many authors presented satisfactory results using rigid flat plates (e.g., Bimbard et al 2013;Yokoyama et al 2013;Yang 2015, 2016;Chang et al 2020;Suzuki et al, 2022). As Lin et al (2021) also suggested, it can be expected that the use of rigid flat plates does not affect a butterfly's natural flight trend. We assume the left wing has the same shape as the right wing.…”
Section: Numerical Modeling Of Butterflymentioning
confidence: 99%
“…In addition to the above-mentioned experimental measurements, some numerical simulations using computational fluid dynamics (CFD) aided by experimental measurements have been conducted (e.g., takeoff of Pieris melete by Sunada et al, 1993; forward flight of Vanessa cardui by Zheng et al, 2013; forward flight of Chilasa clytia by Zhang et al, 2021; forward-climbing flight of Danaus plexipus by Tejaswi et al, 2021; forward flight of Tirumala septentrionis by Lin et al, 2021). Among such numerical simulations, only a few studies have considered the interaction among the wings, body, and ambient air by directly calculating the incompressible Navier-Stokes equations and the equations of the butterfly motion.…”
Section: Introductionmentioning
confidence: 99%
“…In addition, the aspect ratio, wing loading, and flapping frequency were chosen so that these were close to the range of real butterflies. (26,27) Moreover, the effects of the vein structures of the real butterfly wings were not considered and are one of our on-going research topics. (28,29) The body frame is constructed using an acrylic resin (AR-M2), designed with CAD software (Fusion360, Autodesk), and fabricated using a 3D printer (AGILISTA-3200, Keyence).…”
Section: Butterfly-inspired Flapping Wing Robot Designmentioning
confidence: 99%