2014
DOI: 10.1088/0169-5983/47/1/015505
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Free flight simulations of a dragonfly-like flapping wing-body model using the immersed boundary-lattice Boltzmann method

Abstract: Free flights of the dragonfly-like flapping wing-body model are numerically investigated using the immersed boundary-lattice Boltzmann method. The governing parameters of the problem are the Reynolds number Re, the Froude number Fr, and the non-dimensional mass m, and we set the parameters at Re = 200, Fr = 15, and m = 51. First, we simulate free flights of the model without the pitching rotation for various values of the phase lag angle ϕ between the forewing and the hindwing motions. We find that the wing-bo… Show more

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Cited by 19 publications
(32 citation statements)
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“…The authors also proposed a new IB-LBM (Suzuki & Inamuro 2011), which is more accurate for satisfying the no-slip boundary condition at a moving boundary than other IB-LBMs. The IB-LBM (Suzuki & Inamuro 2011) has already been applied to researches on flows and lift generation by the 2D symmetric flapping wing (Ota et al 2012;Kimura et al 2014) and by a dragonfly-like flapping wing-body model (Minami et al 2015).…”
Section: Introductionmentioning
confidence: 99%
“…The authors also proposed a new IB-LBM (Suzuki & Inamuro 2011), which is more accurate for satisfying the no-slip boundary condition at a moving boundary than other IB-LBMs. The IB-LBM (Suzuki & Inamuro 2011) has already been applied to researches on flows and lift generation by the 2D symmetric flapping wing (Ota et al 2012;Kimura et al 2014) and by a dragonfly-like flapping wing-body model (Minami et al 2015).…”
Section: Introductionmentioning
confidence: 99%
“…Hirohashi and Inamuro 42 have numerically examined targeting and hovering flights of a dragonfly-like flapping wing-body model (Minami et al. 43 ) by using the immersed boundary-lattice Boltzmann method. First, they simulated free flights of the model for various phase angles between the forewing and the hindwing movements and for different stroke angles between the stroke plane and the horizontal plane.…”
Section: Dragonfly Flightsmentioning
confidence: 99%
“…In this paper, the Multi Direct Forcing Method (MDFM) proposed by Wang et al [28] and later coupled with LBM by Suzuki and Inamuro [29] is employed, which improves accuracy of the no-slip boundary condition by solving the body force iteratively. It has been validated with experimental and theoretical results [29,30], and was used in the simulation of butterfly-like and dragonfly-like flapping wings [31].…”
Section: Introductionmentioning
confidence: 99%