2020
DOI: 10.1016/j.taml.2020.01.056
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Influence of wing flexibility on the aerodynamic performance of a tethered flapping bumblebee

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Cited by 5 publications
(10 citation statements)
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“…To resolve the self-oscillation paradox, D. melanogaster wing flexibility would have to reduce drag forces (cΩ 2 ) to below half of current estimates, maintaining roughly equivalent lift. The flexibility observed in D. melanogaster wings during flight is not large [32,57]; and existing studies of insectoid flexible flapping wings indicate reductions in drag-per-lift of up to approximately 20% in the very best cases [58][59][60]. As such, wing flexibility could contribute slightly to resolving the self-oscillation paradox in D. melanogaster, but does not offer a complete resolution.…”
Section: Resolution Of the Self-oscillation Paradox Via Muscular Nonl...mentioning
confidence: 91%
“…To resolve the self-oscillation paradox, D. melanogaster wing flexibility would have to reduce drag forces (cΩ 2 ) to below half of current estimates, maintaining roughly equivalent lift. The flexibility observed in D. melanogaster wings during flight is not large [32,57]; and existing studies of insectoid flexible flapping wings indicate reductions in drag-per-lift of up to approximately 20% in the very best cases [58][59][60]. As such, wing flexibility could contribute slightly to resolving the self-oscillation paradox in D. melanogaster, but does not offer a complete resolution.…”
Section: Resolution Of the Self-oscillation Paradox Via Muscular Nonl...mentioning
confidence: 91%
“…The flexible wing models provide important insights into the influence of flexibility on the aerodynamic performance of insects. The study [64] compared the aerodynamic forces and the power requirements between tethered bumblebees with highly flexible, flexible and rigid wings. The visualization in Figure 9 shows a FluSI computation of a tethered bumblebee with flapping flexible wings.…”
Section: Flexible Wingsmentioning
confidence: 99%
“…Hence, we add 'cross-springs' (Fig. 1G) to give the membrane a slight bending stiffness [25]. This latter suppresses artifacts at the trailing edge of the wing where no discernible vein supports the membrane.…”
Section: Mass-spring Model For Elastic Wingsmentioning
confidence: 99%
“…In the relevant range of the Reynolds numbers (75-4000), wing deformation is caused mainly by the static pressure and the viscous fluid tension is considered negligible [48][49][50]. For timestepping, the coupled fluid-solid system is advanced by employing a semi-implicit staggered scheme, as explained in [25]. On the one hand, we advance the fluid by using the second order Adams-Bashforth (AB2) scheme.…”
Section: Coupling Between the Wing Model And The Fluid Solver For Flu...mentioning
confidence: 99%