TY - GEN
T1 - An implicit, reconstructed discontinuous galerkin method for the unsteady compressible navier-stokes equations on 3D hybrid grids
AU - Xia, Yidong
AU - Luo, Hong
AU - Wang, Chuanjin
AU - Nourgaliev, Robert
PY - 2014
Y1 - 2014
N2 - An implicit, third-order, reconstructed discontinuous Galerkin method, namely RDG (P1P2), is presented for time-accurate solutions to the compressible Navier-Stokes equations on 3D hybrid grids. The spatial discretization is carried out using a Taylor-basis discontinuous Galerkin method, in which a quadratic polynomial (P2) solution is reconstructed via a WENO (P1P2) reconstruction scheme from the underlying linear polynomial discontinuous Gakerkin (P1) solution in each cell for evaluating the fluxes. A series of Explicit first stage, Single Diagonal coefficient, diagonally Implicit Runge-Kutta schemes (termed ESDIRK) are applied for temporal discretization to the resulting ordinary differential equations. The resulting non-linear system of equations at each stage is solved using an approximate Newton's method, in which an LU-SGS preconditioned GMRES solver is applied for the solution to the linear system of equations. The developed code is applied to compute a series of benchmark test cases, including the implicit large eddy simulation of a turbulent lid driven cavity. The numerical results indicate that the use of ESDIRK schemes leads to remarkable improvement in solution efficiency and temporal accuracy over its explicit counterpart. In addition, this implicit RDG (P1P2) method requires much less storage and computing time than the implicit DG (P2) method, resulting in a fast, third-order implicit discontinuous Galerkin method for computing unsteady flow problems.
AB - An implicit, third-order, reconstructed discontinuous Galerkin method, namely RDG (P1P2), is presented for time-accurate solutions to the compressible Navier-Stokes equations on 3D hybrid grids. The spatial discretization is carried out using a Taylor-basis discontinuous Galerkin method, in which a quadratic polynomial (P2) solution is reconstructed via a WENO (P1P2) reconstruction scheme from the underlying linear polynomial discontinuous Gakerkin (P1) solution in each cell for evaluating the fluxes. A series of Explicit first stage, Single Diagonal coefficient, diagonally Implicit Runge-Kutta schemes (termed ESDIRK) are applied for temporal discretization to the resulting ordinary differential equations. The resulting non-linear system of equations at each stage is solved using an approximate Newton's method, in which an LU-SGS preconditioned GMRES solver is applied for the solution to the linear system of equations. The developed code is applied to compute a series of benchmark test cases, including the implicit large eddy simulation of a turbulent lid driven cavity. The numerical results indicate that the use of ESDIRK schemes leads to remarkable improvement in solution efficiency and temporal accuracy over its explicit counterpart. In addition, this implicit RDG (P1P2) method requires much less storage and computing time than the implicit DG (P2) method, resulting in a fast, third-order implicit discontinuous Galerkin method for computing unsteady flow problems.
UR - https://www.scopus.com/pages/publications/85088721625
U2 - 10.2514/6.2014-3220
DO - 10.2514/6.2014-3220
M3 - Conference contribution
AN - SCOPUS:85088721625
SN - 9781624102936
T3 - AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference
BT - AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference 2014
Y2 - 16 June 2014 through 20 June 2014
ER -