2020
DOI: 10.1016/j.euromechflu.2019.08.007
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An investigation of kinematic parameters and stroke function on stroke reversal for three-dimensional vortex structures around a flapping insect wing

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Cited by 4 publications
(5 citation statements)
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“…During hovering, the wing with phase flap (alula) provides the maximum lift but the lowest performance and a stabilizing effect on the LEV [ 159 ]. For a flapping drosophila, at high stroke amplitude, a hairpin-like vortex loop and stroke reversal affect the instant time the wake capture materializes [ 160 ]. Insects even compensate for wing damage.…”
Section: Unique Kinematic Patterns and Wing Flexibilitymentioning
confidence: 99%
“…During hovering, the wing with phase flap (alula) provides the maximum lift but the lowest performance and a stabilizing effect on the LEV [ 159 ]. For a flapping drosophila, at high stroke amplitude, a hairpin-like vortex loop and stroke reversal affect the instant time the wake capture materializes [ 160 ]. Insects even compensate for wing damage.…”
Section: Unique Kinematic Patterns and Wing Flexibilitymentioning
confidence: 99%
“…2020; Lee et al. 2020). In a numerical study with optimization function, Kamisawa and Isogai showed that from hovering to fast forward flight to keep the necessary power minimal, the stroke plane angle should gradually increase (from about 8° to 88°) together with the wing phasing (from about 30° to 90° hindwing lead), while the rate of twist decreases, and the flapping amplitude of the forewing and the hindwing varies as 30°–60° and 20°–40° respectively (Kamisawa & Isogai 2008).…”
Section: Introductionmentioning
confidence: 99%
“…Studies have shown that a small change in the flapping motion of wings may lead to a large change in aerodynamic force generation (Sane & Dickinson 2001;Altshuler et al 2005;Shyy et al 2010). Recently, it has been shown that for a flapping winged system not only the range and timing (Lee, Jang & Lee 2020) of kinematic motions but the complex waveforms can influence the leading-edge vortex (LEV) formation and added mass effects (Bhat et al 2020;Lee et al 2020). In a numerical study with optimization function, Kamisawa and Isogai showed that from hovering to fast forward flight to keep the necessary power minimal, the stroke plane angle should gradually increase (from about 8°to 88°) together with the wing phasing (from about 30°t o 90°hindwing lead), while the rate of twist decreases, and the flapping amplitude of the forewing and the hindwing varies as 30°-60°and 20°-40°respectively (Kamisawa & Isogai 2008).…”
Section: Introductionmentioning
confidence: 99%
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“…Several authors [9][10][11] showed how the aerodynamic coefficients (including the slope of the lift coefficient) of flexible micro air vehicle (MAV) wings of low aspect ratio at low Reynolds number can either grow or decrease depending on the geometry of the wing and the settings of flexible parts. Furthermore, the aerodynamic performance of flexible wings under flapping conditions (typical of bio-inspired UAVs) and the influence of their aspect ratio have also attracted attention lately [12][13][14][15][16].…”
Section: Introductionmentioning
confidence: 99%