4 research outputs found
Coupling of hybridisable discontinuous Galerkin and finite volumes for transient compressible flows
Fast, high-fidelity solution workflows for transient flow phenomena is an important challenge in the computational fluid dynamics (CFD) community. Current low-order methodologies suffer from large dissipation and dispersion errors and require large mesh sizes for unsteady flow simulations. Recently, on the other hand, high-order methods have gained popularity offering high solution accuracy. But they suffer from the lack of robust, curvilinear mesh generators.A novel methodology that combines the advantages of the classical vertex-centred finite volume (FV) method and high-order hybridisable discontinuous Galerkin (HDG) method is presented for the simulation of transient inviscid compressible flows. The resulting method is capable of simulating the transient effects on coarse, unstructured meshes that are suitable to perform steady simulations with traditional low-order methods. In the vicinity of the aerodynamic shapes, FVs are used whereas in regions where the size of the element is too large for finite volumes to provide an accurate answer, the high-order HDG approach is employed with a non-uniform degree of approximation. The proposed method circumvents the need to produce tailored meshes for transient simulations, as required in a low-order context, and also the need to produce high-order curvilinear meshes, as required by high-order methods.FV and HDG methods for compressible inviscid flows with an implicit time-stepping method and capable of handling flow discontinuities is developed. A two-way coupling of the methods in a monolithic manner was achieved by the consistent application of the so-called transmission conditions at the FV-HDG interface. Numerical tests highlight the optimal convergence properties of the coupled HDG-FV scheme. Numeri-cal examples demonstrate the potential and suitability of the developed methodology for unsteady 2D and 3D flows in the context of simulating the wind gust effect on aerodynamic shapes
Orthogonal subgrid-scale stabilization for nonlinear reaction-convection-diffusion equations
Nonlinear reaction-convection-diffusion equations are encountered in
modeling of a variety of natural phenomena such as in chemical reactions,
population dynamics and contaminant dispersal. When the
scale of convective and reactive phenomena are large, Galerkin finite
element solution fails.
As a remedy, Orthogonal Subgrid Scale stabilization is applied to the
finite element formulation. It has its origins in the Variational Multi
Scale approach. It is based on a fine grid - coarse grid component sum
decomposition of solution and utilizes the fine grid solution orthogonal
to the residual of the finite element coarse grid solution as a correction
term. With selective mesh refinement, a stabilized oscillation-free
solution that can capture sharp layers is obtained. Newton Raphson
method is utilized for the linearization of nonlinear reaction terms.
Backward difference scheme is used for time integration.
The formulation is tested for cases with standalone and coupled systems
of transient nonlinear reaction-convection-diffusion equations.
Method of manufactured solution is used to test for correctness and
bug-free implementation of the formulation. In the error analysis,
optimal convergence is achieved. Applications in channel flow, cavity
flow and predator-prey model is used to highlight the need and
effectiveness of the stabilization technique
A coupled HDG-FV scheme for the simulation of transient inviscid compressible flows
A methodology that combines the advantages of the vertex-centred finite volume (FV) method and high-order hybridisable discontinuous Galerkin (HDG) method is presented for the simulation of the transient inviscid two dimensional flows. The resulting method is suitable for simulating the transient effects on coarse meshes that are suitable to perform steady simulations with traditional low-order methods. In the vicinity of the aerodynamic shapes, FVs are used whereas in regions where the size of the element is too large for finite volumes to provide an accurate answer, the high-order HDG approach is employed with a non-uniform degree of approximation. The proposed method circumvents the need to produce tailored meshes for transient simulations, as required in a low-order context, and also the need to produce high-order curvilinear meshes, as required by high-order methods. Numerical examples are used to test the optimal convergence properties of the combined HDG-FV scheme and to demonstrate its potential in the context of simulating the wind gust effect on aerodynamic shapes
Orthogonal subgrid-scale stabilization for nonlinear reaction-convection-diffusion equations
Nonlinear reaction-convection-diffusion equations are encountered in
modeling of a variety of natural phenomena such as in chemical reactions,
population dynamics and contaminant dispersal. When the
scale of convective and reactive phenomena are large, Galerkin finite
element solution fails.
As a remedy, Orthogonal Subgrid Scale stabilization is applied to the
finite element formulation. It has its origins in the Variational Multi
Scale approach. It is based on a fine grid - coarse grid component sum
decomposition of solution and utilizes the fine grid solution orthogonal
to the residual of the finite element coarse grid solution as a correction
term. With selective mesh refinement, a stabilized oscillation-free
solution that can capture sharp layers is obtained. Newton Raphson
method is utilized for the linearization of nonlinear reaction terms.
Backward difference scheme is used for time integration.
The formulation is tested for cases with standalone and coupled systems
of transient nonlinear reaction-convection-diffusion equations.
Method of manufactured solution is used to test for correctness and
bug-free implementation of the formulation. In the error analysis,
optimal convergence is achieved. Applications in channel flow, cavity
flow and predator-prey model is used to highlight the need and
effectiveness of the stabilization technique