Higher Order Multigrid Algorithms for a 2D and 3D RANS-kω DG-Solver
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1 Folie 1 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Higher Order Multigrid Algorithms for a 2D and 3D RANS-kω DG-Solver Marcel Wallraff, Tobias Leicht DLR Braunschweig (AS - C 2 A 2 S 2 E)
2 Folie 2 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Multigrid algorithms
3 Folie 3 > HONOM 2013 > Marcel Wallraff, Tobias Leicht DG discretization Basis functions non-parametric ortho-normal basis functions directly formulated in physical space also referred to as Taylor-DG need to be evaluated for each mesh element RANS-kω equations kω turbulence model second scheme of Bassi and Rebay (BR2) for the viscous terms Roe flux as a convective flux, based on an eigen-decomposition of the full jacobian
4 Folie 4 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Non-linear multigrid method nested hierarchy of linear spaces V lmin V lmin +1 V lmax 1 V lmax R n l min R n l min +1 R n lmax 1 R n lmax intergrid transfer operators: prolongation: natural injection Il 1 l : Rn l 1 R n l ( ) canonical restriction operator I l 1 := I l l 1 l non-linear multigrid algorithm also requires: restricted nonlinear state vector: orthogonal L 2 -projection Îl 1 on the space V l l 1
5 Folie 5 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Non-linear multigrid method Let the non-linear problem to be solved on the fine level l max be given by L lmax (u lmax ) = f lmax. restrict solution approximation u l 1 := Îl 1 u l l compute forcing function for the coarse level: f l 1 f l 1 + I l 1 (f l l L l (u l )) Galerkin-transfer for the Jacobian: R l 1 = I l 1 l (f l 1 L l 1 (u 0 l 1 ) ) R l I l l 1
6 Folie 6 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Non-linear smoother / solver smoother / solver linearized Backward-Euler Solve [ (α i t) 1 M + R l ] (ul,i u l,i 1 ) = [ f l L l (u l,i 1 ) ], where R l is the fully implicit Jacobian matrix and M is the mass matrix. In addition to that u l,j is a state vector, with u l,j V l j N. local pseudo-time steps, adaptive CFL number
7 Folie 7 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Linear smoother / solver Krylov method as linear solver (GMRES method) line-jacobi as preconditioner / smoother let L l,k (u l,k ) = f l,k the underlying linear problem on line k, solve δu l,k,i := u l,k,i u l,k,i 1 = R 1 l,k (f l,k L l,k u l,k,i 1 ) set u l,k,i := u l,k,i 1 + δu l,k,i, where R 1 l,k is the inverse of the Jacobian matrix computed one line k in the mesh
8 Folie 8 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Relaxation scheme Jacobian / system matrix structure element diagonal line neighbor off-line off-diagonal matrix blocks
9 Folie 9 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Numerical algorithms possible solver choices single grid Backward-Euler start up streategy in mesh or order sequencing for improved initial conditions linear MG as preconditioner non-linear MG to accelerate process in pseudo-time non-linear MG with linear MG on each level
10 Folie 10 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Numerical parameters for the non-linear problems non-linear multigrid only V-cycles will be presented one pre- and post-smoothing iteration on each level one smoothing iteration on the lowest level a linearized Backward-Euler scheme as smoother using an SER time steping scheme for the Backward-Euler Galerkin-transfer to obtain the Jacobian on the lower levels
11 Folie 11 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Numerical parameters for the linear problems parameters for solving the resulting linear problems on every level from the Backward-Euler linearization GMRES method with a fixed number of max steps on every level linear multigrid as a preconditioner for the GMRES method one V-cycle is done for preconditioning no pre-smoothing iterations four post-smoothing iterations four smoothing iterations on the lowest level line-jacobi scheme as smoother Galerkin-transfer to obtain the lower level matrices
12 Folie 12 > HONOM 2013 > Marcel Wallraff, Tobias Leicht L1T2 high-lift configuration flow conditions: Mach: Reynolds number: 3,520,000 α = testcase from EC funded ADIGMA project computations will be shown on an unstructured mesh with mixed elements p = 2 solution is desired for all computations
13 Folie 13 > HONOM 2013 > Marcel Wallraff, Tobias Leicht L1T2 high-lift configuration mixed-element mesh (CENAERO via GMSH) third order DoF three levels
14 Folie 14 > HONOM 2013 > Marcel Wallraff, Tobias Leicht L1T2 high-lift configuration run time comparison: h-mg density residual SG h-sequence h-nmg h-lmg h-nmg + LMG normalized CPU time
15 Folie 15 > HONOM 2013 > Marcel Wallraff, Tobias Leicht L1T2 high-lift configuration run time comparison: p-mg density residual SG p-sequence p-nmg p-lmg p-nmg + LMG normalized CPU time
16 Folie 16 > HONOM 2013 > Marcel Wallraff, Tobias Leicht VFE-2 Delta-Wing with rounded leading edge flow conditions: Mach: 0.4 Reynolds number: 3,000,000 α = 13.3, β = 0 testcase from EC funded IDIHOM project computations will be shown on a structured mesh with elements p = 2 solution is desired for all computations
17 Folie 17 > HONOM 2013 > Marcel Wallraff, Tobias Leicht VFE-2 Delta-Wing with rounded leading edge original FV mesh with elements was two times agglomerated resulting in a higher order mesh with curved elements geometry original mesh curved mesh with faces with straight faces represented by polynomials of order 4
18 Folie 18 > HONOM 2013 > Marcel Wallraff, Tobias Leicht VFE-2 Delta-Wing with rounded leading edge density residual h-sequence h-lmg h-nmg h-nmg + LMG p-sequence p-lmg p-nmg p-nmg + LMG top level non-linear iterations
19 Folie 19 > HONOM 2013 > Marcel Wallraff, Tobias Leicht VFE-2 Delta-Wing with rounded leading edge density residual h-nmg + LMG h-nmg + LMG p-nmg + LMG p-nmg + LMG top level non-linear iterations
20 Folie 20 > HONOM 2013 > Marcel Wallraff, Tobias Leicht VFE-2 Delta-Wing with rounded leading edge The blue computation on the mesh with elements and the red computation on an adjoint refined mesh with elemtents. density residual p-nmg + LMG p-nmg + LMG V-cycle
21 Folie 21 > HONOM 2013 > Marcel Wallraff, Tobias Leicht Thanks for your attention!
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