2008Aeronautical Computing TechniqueRequires access

High Order Discontinuous Galerkin Method for Solving Euler Equations on Unstructured Grids

He-Yong Xu

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Abstract

The main purpose of this paper is to develop a discontinuous Galerkin method suitable for the numerical solution of the Euler equations on unstructured grids.Based on the theory of discontinuous Galerkin method,the approximate solution within each element is expanded in a series of local polynomials bases functions;the numerical flux of Euler equations are calculated by using the Gaussian quadrature rules and Roe scheme;and time is advanced by explicit fourth-order accurate Runge-Kutta method.The versatility of the discontinuous Galerkin method to obtain high-order accurate solutions in realistic geometries is demonstrated with the results obtained for subsonic and transonic inviscid flow over a NACA-0012 airfoil and low speed inviscid flow around a 2D cylinder.The Numerical results indicate that the presented discontinuous Galerkin method has properties of good convergence speed,smaller numerical dissipation and excellent ability to capture shocks.

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What this paper is about

The main purpose of this paper is to develop a discontinuous Galerkin method suitable for the numerical solution of the Euler equations on unstructured grids.Based on the theory of discontinuous Galerkin method,the approximate solution within each element is expanded in a series of local polynomials bases functions;the numerical flux of Euler equations are calculated by using the Gaussian quadrature rules and Roe scheme;and time is advanced by explicit fourth-order accurate Runge-Kutta method.The versatility of the discontinuous Galerkin method to obtain high-order accurate solutions in realistic geometries is demonstrated with the results obtained for subsonic and transonic inviscid flow over a NACA-0012 airfoil and low speed inviscid flow around a 2D cylinder.The Numerical results indicate that the presented discontinuous Galerkin method has properties of good convergence speed,smaller numerical dissipation and excellent ability to capture shocks.

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Available abstract

The main purpose of this paper is to develop a discontinuous Galerkin method suitable for the numerical solution of the Euler equations on unstructured grids.Based on the theory of discontinuous Galerkin method,the approximate solution within each element is expanded in a series of local polynomials bases functions;the numerical flux of Euler equations are calculated by using the Gaussian quadrature rules and Roe scheme;and time is advanced by explicit fourth-order accurate Runge-Kutta method.The versatility of the discontinuous Galerkin method to obtain high-order accurate solutions in realistic geometries is demonstrated with the results obtained for subsonic and transonic inviscid flow over a NACA-0012 airfoil and low speed inviscid flow around a 2D cylinder.The Numerical results indicate that the presented discontinuous Galerkin method has properties of good convergence speed,smaller numerical dissipation and excellent ability to capture shocks.

Key concepts: Discontinuous Galerkin method, Inviscid flow, Transonic, Euler equations, Mathematics, Airfoil, Galerkin method, NACA airfoil

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