2015
DOI: 10.1016/j.jcp.2014.10.045
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A partitioned scheme for fluid–composite structure interaction problems

Abstract: We present a benchmark problem and a loosely-coupled partitioned scheme for fluidstructure interaction with composite structures. The benchmark problem consists of an incompressible, viscous fluid interacting with a structure composed of two layers: a thin elastic layer with mass which is in contact with the fluid and modeled by the Koiter membrane/shell equations, and a thick elastic layer with mass modeled by the equations of linear elasticity. An efficient, modular, partitioned operator-splitting scheme is … Show more

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Cited by 54 publications
(41 citation statements)
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“…This is consistent with the experimental measurements of the aortic diameters reported by Wolak et al (2008) and O’Rourke and Nichols (2005). The blood density is taken to be ρ f = 1 g/cm 3 and viscosity μ f = 0.035 g/cm s. We impose symmetry boundary conditions at the fluid bottom boundary normalΓbf (see Figure 1) (Khanafer and Berguer (2009), Bukač et al (2015)). …”
Section: Methodsmentioning
confidence: 53%
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“…This is consistent with the experimental measurements of the aortic diameters reported by Wolak et al (2008) and O’Rourke and Nichols (2005). The blood density is taken to be ρ f = 1 g/cm 3 and viscosity μ f = 0.035 g/cm s. We impose symmetry boundary conditions at the fluid bottom boundary normalΓbf (see Figure 1) (Khanafer and Berguer (2009), Bukač et al (2015)). …”
Section: Methodsmentioning
confidence: 53%
“…To circumvent the issues related to the motion of the fluid domain due to the fluid-structure interaction, we use the Navier-Stokes equations in the ALE form (Donea (1983), Duarte et al (2004), Bukač et al (2015)). …”
Section: Methodsmentioning
confidence: 99%
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“…Examples of this type of systems are quite common in engineering, like floating structures, wind turbines, man-made drones and in the study of biological systems such as artery or heart valves. In literature these topics are investigated deeply and the interested reader can see [9,10,11,12,13,14]. Many attempts to use optimization techniques can be found, for example in [15], where the authors propose a solution method for the problem of optimizing a non-linear aeroelasticity system in a steady-state flow by using a sensitivity method.…”
Section: Introductionmentioning
confidence: 99%