A computational fluid dynamics of `clap and fling' in the smallest insects
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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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].”
From Reynolds number limits for jet propulsion: a numerical study of simplified jellyfish (2011) · cites this paper as [27]
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Fang, F., Ho, K. L., Ristroph, L., & Shelley, M. (2017) · Journal of Fluid Mechanics · doi:10.1017/jfm.2017.150 · Cited by 28 · see citing works
Naut Your Everyday Jellyfish Model: Exploring How Tentacles and Oral Arms Impact Locomotion
Miles, J. G., & Battista, N. (2019) · Fluids · doi:10.3390/fluids4030169 · Cited by 28 · see citing works
Aeromechanics in aeroecology: flight biology in the aerosphere
Swartz, S. M., Breuer, K., & Willis, D. J. (2007) · Integrative and Comparative Biology · doi:10.1093/icb/icn054 · Cited by 27 · see citing works
Interactions of the wakes of two flapping wings in hover
Han, J.-S., Kim, H.-Y., & Han, J. (2019) · Physics of Fluids · doi:10.1063/1.5078669 · Cited by 27 · see citing works
Determination of the wingsnap sonation mechanism of the Golden-collared manakin (Manacus vitellinus)
Bodony, D. J., Day, L. B., Friscia, A. R., Fusani, L., Kharon, A., Swenson, G. W., Wikelski, M. C., & Schlinger, B. A. (2016) · Journal of Experimental Biology · doi:10.1242/jeb.128231 · Cited by 26 · see citing works
Recent advancements in flapping mechanism and wing design of micro aerial vehicles
Yousaf, R., Shahzad, A., Qadri, M. N. M., & Javed, A. (2020) · Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science · doi:10.1177/0954406220960783 · Cited by 26 · see citing works
Maniyeri, R., & Kang, S. (2014) · Applied Mathematical Modelling · doi:10.1016/j.apm.2013.11.059 · Cited by 26 · see citing works
A study of different modeling choices for simulating platelets within the immersed boundary method
Shankar, V., Wright, G. B., Fogelson, A. L., & Kirby, R. M. (2012) · Applied Numerical Mathematics · doi:10.1016/j.apnum.2012.09.006 · Cited by 24 · see citing works
Ishihara, D. (2022) · Fluids · doi:10.3390/fluids7010026 · Cited by 24 · see citing works
Flow within models of the vertebrate embryonic heart
Santhanakrishnan, A., Nguyen, N. L. U., Cox, J. G., & Miller, L. A. (2009) · Journal of Theoretical Biology · doi:10.1016/j.jtbi.2009.04.020 · Cited by 24 · see citing works
- 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
- Publisher
- The Company of Biologists
- 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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