A mixed volume grid approach for the Euler and Navier-Stokes equations
Author(s) -
William J. Coirier,
Philip C. E. Jorgenson
Publication year - 1996
Publication title -
38th aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1996-762
Subject(s) - hexahedron , laminar flow , tetrahedron , polyhedron , polygon mesh , inviscid flow , quadrilateral , regular grid , euler's formula , euler equations , cartesian coordinate system , mesh generation , discretization , grid , volume mesh , geometry , unstructured grid , series (stratigraphy) , finite volume method , mathematics , mathematical analysis , finite element method , mechanics , physics , paleontology , biology , thermodynamics
An approach for solving the compressible Euler and Navier-Stokes equations upon meshes composed of nearly arbitrary polyhedra is described. Each polyhedron is constructed from an arbitrary number of triangular and quadrilateral face elements, allowing the unified treatment of tetrahedral, prismatic, pyramidal, and hexahedral cells, as well the general cut cells produced by Cartesian mesh approaches. The basics behind the numerical approach and the resulting data structures are described. The accuracy of the mixed volume grid approach is assessed by performing a grid refinement study upon a series of hexahedral, tetrahedral, prismatic, and Cartesian meshes for an analytic inviscid problem. A series of laminar validation cases are made, comparing the results upon differing grid topologies to each other, to theory, and experimental data. A computation upon a prismatic/tetrahedral mesh is made simulating the laminar flow over a wall/cylinder combination.
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