Abstract:Numerical methods are presented for the simulation of steady and unsteady micro gas¯ows with moving boundaries found in micro scale¯uidic devices. Both steady and unsteady¯ows are calculated by using an implicit real-time discretization and a dual-time stepping scheme implemented in a high-order upwind ®nite-volume unstructured-grid Navier±Stokes solver. For moving boundary problems, a new dynamic mesh method has been developed which is shown to be robust in handling large mesh deformation. Micro-scale¯ows stu… Show more
“…Luo and Pedley [1][2][3] performed a time-dependent simulation of a coupled flow-membrane problem, using the Arbitrary Lagrangian Eulerian (ALE) method together with a spine scheme to treat a compliant wall moving in its wall normal direction in a channel. Zhao et al [4,5] have also proposed a new dynamic mesh scheme to simulate an arbitrarily moving elastic wall in a similar channel based on the ALE. Gaitonde [6,7] developed a moving mesh method for the computation of compressible viscous flow past moving aerofoils.…”
“…Luo and Pedley [1][2][3] performed a time-dependent simulation of a coupled flow-membrane problem, using the Arbitrary Lagrangian Eulerian (ALE) method together with a spine scheme to treat a compliant wall moving in its wall normal direction in a channel. Zhao et al [4,5] have also proposed a new dynamic mesh scheme to simulate an arbitrarily moving elastic wall in a similar channel based on the ALE. Gaitonde [6,7] developed a moving mesh method for the computation of compressible viscous flow past moving aerofoils.…”
“…We found the finite element vertex-based mesh motion solver to produce superior numerical results, as compared with some of the other popular mesh motion methods (e.g. the spring analogy [28,29] and its variants [30,31,32,33]), as it guarantees boundedness in the Laplacian operator (the Laplace equation governs mesh vertex motion), even when the fluid cells approach a degenerate state [34,20]. This feature is vital for FSI simulations involving large structural displacements; since such structural responses could lead to considerable deformation and skewness of the attached fluid control volumes.…”
A high fidelity fluid-structure interaction simulation may require many days to run, on hundreds of cores. This poses a serious burden, both in terms of time and economic considerations, when repetitions of such simulations may be required (e.g. for the purpose of design optimization). In this paper we present strategies based on (constrained) Bayesian optimization (BO) to alleviate this burden. BO is a numerical optimization technique based on Gaussian processes (GP) that is able to efficiently (with minimal calls to the expensive FSI models) converge towards some globally optimal design, as gauged using a black box objective function. In this study we present a principled design evolution that moves from FSI model verification, through a series of Bridge Simulations (bringing the verification case incrementally closer to the application), in order that we may identify material properties for an underwater, unmanned, autonomous vehicle (UUAV) sail plane. We are able to achieve fast convergence towards an optimal design, using a small number of FSI simulations (a dozen at most), even when selecting over several design parameters, and while respecting optimization constraints.
“…In cases of small amplitude motion, the deforming grid technique could be used. In MaPFlow the nodes of the mesh are moved based on a damping term as described in [52].…”
Modeling free surface flows in a CFD context typically requires an incompressible approach along with a formulation to account for the air–water interface. Commonly, pressure-correction algorithms combined with the Volume of Fluid (VOF) method are used to describe these kinds of flows. Pressure-correction algorithms are segregated solvers, which means equations are solved in sequence until convergence is accomplished. On the contrary, the artificial compressibility (AC) method solves a single coupled system of equations. Solving at each timestep a single system of equations obviates the need for segregated algorithms, since all equations converge simultaneously. The goal of the present work is to combine the AC method with VOF formulation and prove its ability to account for unsteady flows of immiscible fluids. The presented system of equations has a hyperbolic nature in pseudo-time, thus the arsenal of the hyperbolic discretization process can be exploited. To this end, a thorough investigation of unsteady flows is presented to demonstrate the ability of the method to accurately describe unsteady flows. Problems of wave propagation on constant and variable bathymetry are considered, as well as a fluid structure interaction problem, where viscous effects have a significant impact on the motion of the structure. In all cases the results obtained are compared with theoretical or experimental data. The straightforward implementation of the method, as well as its accurate predictions, shows that AC method can be regarded as a suitable choice to account for free surface flows.
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.