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A multigrid accelerated hybrid unstructured mesh method for 3D compressible turbulent flow
Authors:K A Sørensen  O Hassan  K Morgan  N P Weatherill
Affiliation:(1) Aerodynamics-MT632, EADS, Military Aircraft, 81663 München, Germany, DE;(2) Civil & Computational Engineering Centre, University of Wales, Swansea SA2 8PP, Wales, UK, GB
Abstract: A cell vertex finite volume method for the solution of steady compressible turbulent flow problems on unstructured hybrid meshes of tetrahedra, prisms, pyramids and hexahedra is described. These hybrid meshes are constructed by firstly discretising the computational domain using tetrahedral elements and then by merging certain tetrahedra. A one equation turbulence model is employed and the solution of the steady flow equations is obtained by explicit relaxation. The solution process is accelerated by the addition of a multigrid method, in which the coarse meshes are generated by agglomeration, and by parallelisation. The approach is shown to be effective for the simulation of a number of 3D flows of current practical interest. Sponsored by The Research Council of Norway, project number 125676/410 Dedicated to the memory of Prof. Mike Crisfield, a respected colleague
Keywords:  Steady 3D aerodynamic flows  Finite volume method  Hybrid unstructured mesh  One equation turbulence model  Agglomerated          multigrid  Parallelisation
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