2017
DOI: 10.1016/s1672-6529(16)60392-x
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A simulation of the flight characteristics of the deployable hindwings of beetle

Abstract: The University of Gloucestershire accepts no liability for any infringement of intellectual property rights in any material deposited but will remove such material from public view pending investigation in the event of an allegation of any such infringement.

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Cited by 10 publications
(7 citation statements)
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References 37 publications
(35 reference statements)
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“…This turbulence model combines the Wilcox k-ω model and k-ε model by blending functions, using the k-ω model in the near wall region and using the k-ε model in the far field. Therefore it is an effective blend of the high simulation accuracy for separation flow of the k-ω model and the low sensitivity to initial turbulence parameters of the k-ε model, and one of the most widely used turbulence models [21]- [24]. The studies of Ref.…”
Section: B Computational Setup For Cfdmentioning
confidence: 99%
“…This turbulence model combines the Wilcox k-ω model and k-ε model by blending functions, using the k-ω model in the near wall region and using the k-ε model in the far field. Therefore it is an effective blend of the high simulation accuracy for separation flow of the k-ω model and the low sensitivity to initial turbulence parameters of the k-ε model, and one of the most widely used turbulence models [21]- [24]. The studies of Ref.…”
Section: B Computational Setup For Cfdmentioning
confidence: 99%
“…28 Furthermore, the UVLM simply requires the description of the zero-thickness wing surface for aerodynamic calculations, in contrast to other CFD (computational fluid dynamics) solvers which additionally require a fluid domain. 21,29 The UVLM is acceptable for scenarios involving small angles of attack 30 and is based on the assumption that the airflow around the wing is incompressible, irrotational, and inviscid. These assumptions remain valid for the application of interest.…”
Section: Unsteady Vortex Lattice Methodsmentioning
confidence: 99%
“…The shape and size of the bionic model determine that the flight of C. buqueti belongs to an incompressible fluid, and the cuboid is selected as the computational domain. The lengths of approximately 5-10 times wing or 10-20 times mean chord of insects are often taken as the reference to determine the calculation domain [33,34]. In this study, the dimension of the computational domain is 0.3 m in length (approximately 7 times elytron length), 0.36 m in width (approximately 8 times elytron length) and 0.22 m in height (approximately 5 times elytron length).…”
Section: Numerical Simulation Of the Elytra Flappingmentioning
confidence: 99%