On the computation of compressible flows on unstructured hybrid grids

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Abstract

Computation of compressible flows using an unstructured hybrid grid method is presented in this paper. The spatial discretization is carried out using a cell-centered finite volume approximation. The spatially discretized governing equations are integrated in time using a linearized implicit scheme. A fast, matrix-free implicit method, GMRES+LU-SGS, is then applied to solve the resultant system of linear equations. Three open issues related to the cell-centered finite volume formulation: gradient approximation, viscous discretization, and interface value estimation are examined, analyzed, and discussed. It is proven mathematically and demonstrated numerically that an inappropriate treatment of these issues may result in inaccurate and inconsistent numerical solutions to the Navier-Stokes equations on non-uniform grids. An inverse-distance weighted average is proposed to evaluate the flow variables at the cell interfaces, and found to be effective to achieve a consistent convergence on non-uniform grids for the solution of the Navier-Stokes equations on non-uniform and irregular grids.

Original languageEnglish
Title of host publication47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
StatePublished - 2009
Externally publishedYes
Event47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States
Duration: Jan 5 2009Jan 8 2009

Publication series

Name47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Conference

Conference47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Country/TerritoryUnited States
CityOrlando, FL
Period01/5/0901/8/09

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