Multigrid solution of the Euler equations on unstructured and adaptive meshes

作者: Antony Jameson , Dimitri Mavriplis

DOI:

关键词:

摘要: A multigrid algorithm has been developed for solving the steady-state Euler equations in two dimensions on unstructured triangular meshes. The method assumes various coarse and fine grids of sequence to be independent one another, thus decoupling grid generation procedure from algorithm. transfer variables between meshes employs a tree-search which rapidly identifies regions overlap cells. Finer are obtained either by regenerating new globally refined meshes, or adaptively refining previous coarser mesh. For both cases, observed convergence rates comparable those with structured solvers. generated shown produce solutions higher accuracy fewer mesh points.

参考文章(6)
A. Jameson, T. Baker, N. Weatherill, CALCULATION OF IN VISCID TRANSONIC FLOW OVER A COMPLETE AIRCRAFT 24th Aerospace Sciences Meeting. pp. 86- 103 ,(1986) , 10.2514/6.1986-103
A. JAMESON, WOLFGANG SCHMIDT, ELI TURKEL, Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes 14th Fluid and Plasma Dynamics Conference. pp. 1259- 1281 ,(1981) , 10.2514/6.1981-1259
R. Löhner, K. Morgan, An unstructured multigrid method for elliptic problems International Journal for Numerical Methods in Engineering. ,vol. 24, pp. 101- 115 ,(1987) , 10.1002/NME.1620240108
F. ANGRAND, A. DERVIEUX, V. BILLEY, J. PERIAUX, C. POULETTY, 2-D and 3-D Euler flow calculations with a second-order accurate Galerkin finite element method 18th Fluid Dynamics and Plasmadynamics and Lasers Conference. ,(1985) , 10.2514/6.1985-1706
J. DANNENHOFFER, III, J. BARON, ROBUST GRID ADAPTATION FOR COMPLEX TRANSONIC FLOWS. 24th Aerospace Sciences Meeting. ,(1986) , 10.2514/6.1986-495