Cited by 224Biomimetic flight and propulsion mechanismsFluid dynamics and aerodynamics studiesFluid Dynamics and Turbulent Flows

A computational fluid dynamics of `clap and fling' in the smallest insects

Miller, Laura A., Peskin, Charles S.·2005·Journal of Experimental Biology

Abstract

In this paper, we have used the immersed boundary method to solve the two-dimensional Navier-Stokes equations for two immersed wings performing an idealized 'clap and fling' stroke and a 'fling' half-stroke. We calculated lift coefficients as functions of time per wing for a range of Reynolds numbers (Re) between 8 and 128. We also calculated the instantaneous streamlines around each wing throughout the stroke cycle and related the changes in lift to the relative strength and position of the leading and trailing edge vortices. Our results show that lift generation per wing during the 'clap and fling' of two wings when compared to the average lift produced by one wing with the same motion falls into two distinct patterns. For Re=64 and higher, lift is initially enhanced during the rotation of two wings when lift coefficients are compared to the case of one wing. Lift coefficients after fling and during the translational part of the stroke oscillate as the leading and trailing edge vortices are alternately shed. In addition, the lift coefficients are not substantially greater in the two-winged case than in the one-winged case. This differs from three-dimensional insect flight where the leading edge vortices remain attached to the wing throughout each half-stroke. For Re=32 and lower, lift coefficients per wing are also enhanced during wing rotation when compared to the case of one wing rotating with the same motion. Remarkably, lift coefficients following two-winged fling during the translational phase are also enhanced when compared to the one-winged case. Indeed, they begin about 70% higher than the one-winged case during pure translation. When averaged over the entire translational part of the stroke, lift coefficients per wing are 35% higher for the two-winged case during a 4.5 chord translation following fling. In addition, lift enhancement increases with decreasing Re. This result suggests that the Weis-Fogh mechanism of lift generation has greater benefit to insects flying at lower Re. Drag coefficients produced during fling are also substantially higher for the two-winged case than the one-winged case, particularly at lower Re.

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Crossref · 10.1242/jeb.01376

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  • The immersed boundary method has been applied to a wide variety of problems in biological fluid dynamics for intermediate Re including insect flight, aquatic locomotion, and ciliary driven flows.

    “The immersed boundary method has been applied to a wide variety of problems in biological fluid dynamics for intermediate Re including insect flight [26, 27, 28], aquatic locomotion [16, 15], and ciliary driven flows [18].”

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Authors
Miller, L. A., & Peskin, C. S.
Affiliations
  • University of Utah (US)
  • Courant Institute of Mathematical Sciences (US)
Corresponding author
Miller, Laura A.
Venue
Journal of Experimental Biology
Published
2005-01-15
Volume
208
Issue
2
Pages
195-212
ISSN
  • 0022-0949 (ISSN-L)
  • 1477-9145
OpenAlex
W2045343226
Cited by
224
References
25
Citations by year
2026: 5 · 2025: 8 · 2024: 8 · 2023: 3 · 2022: 7 · 2021: 12 · 2020: 10 · 2019: 15 · 2018: 14 · 2017: 21 · 2016: 15 · 2015: 7 · 2014: 13 · 2013: 9 · 2012: 12
FWCI
22.43
Type
journal article
Language
en
Open access
closed
Locations
  • Journal of Experimental Biology (publishedVersion)
  • PubMed (publishedVersion)
  • HighWire Press Open Archive (submittedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Biomimetic flight and propulsion mechanisms
  • Physical Sciences › Engineering › Computational Mechanics › Fluid dynamics and aerodynamics studies
  • Physical Sciences › Engineering › Computational Mechanics › Fluid Dynamics and Turbulent Flows
Keywords
clap-and-fling, insect flight, flapping wings, lift generation, Weis-Fogh mechanism, leading-edge vortex, trailing edge vortex, Reynolds number effects, drag, wing rotation, small insects
MeSH terms
Animals, Biomechanical Phenomena, Computer Simulation, Flight, Animal, Insecta, Models, Theoretical, Wings, Animal

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