An adaptive viscosity regularization approach for the numerical solution of conservation laws: Application to finite element methods
We introduce an adaptive viscosity regularization approach for the numerical solution of systems of nonlinear conservation laws with shock waves. The approach seeks to solve a sequence of regularized problems consisting of the system of conservation laws and an additional Helmholtz equation for the...
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Veröffentlicht in: | Journal of computational physics 2023-12, Vol.494 (C), p.112507, Article 112507 |
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Sprache: | eng |
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Zusammenfassung: | We introduce an adaptive viscosity regularization approach for the numerical solution of systems of nonlinear conservation laws with shock waves. The approach seeks to solve a sequence of regularized problems consisting of the system of conservation laws and an additional Helmholtz equation for the artificial viscosity. We propose a homotopy continuation of the regularization parameters to minimize the amount of artificial viscosity subject to positivity-preserving and smoothness constraints on the numerical solution. The regularization methodology is combined with a mesh adaptation strategy that identifies the shock location and generates shock-aligned meshes, which allows to further reduce the amount of artificial dissipation and capture shocks with increased accuracy. We use the hybridizable discontinuous Galerkin method to numerically solve the regularized system of conservation laws and the continuous Galerkin method to solve the Helmholtz equation for the artificial viscosity. We show that the approach can produce approximate solutions that converge to the exact solution of the Burgers' equation. Finally, we demonstrate the performance of the method on inviscid transonic, supersonic, hypersonic flows in two dimensions. The approach is found to be accurate, robust and efficient, and yields very sharp yet smooth solutions in a few homotopy iterations.
•An adaptive viscosity regularization method is developed for nonlinear conservation laws with shock waves.•It minimizes the amount of artificial viscosity and enforces smoothness constraints on the numerical solution.•It is applied to several inviscid transonic, supersonic, and hypersonic flows.•The method is found to yield accurate, sharp and smooth solutions within a few iterations. |
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ISSN: | 0021-9991 1090-2716 |
DOI: | 10.1016/j.jcp.2023.112507 |