Análisis de Problemas de Flujo Compresible Usando Técnicas de Elementos Finitos y Remallado Adaptivo
Abstract
A set of codes for the analysis of laminar compressible flow in two dimensions -Euler and Navier Stokes
Equations- is presented. The advancing Front Technique with adaptive automatic remeshing has been used to create the meshes and a two step Taylor Galerkin with artificial diffusion techniques to solve the flow. Some examples of supersonic flow are described
Equations- is presented. The advancing Front Technique with adaptive automatic remeshing has been used to create the meshes and a two step Taylor Galerkin with artificial diffusion techniques to solve the flow. Some examples of supersonic flow are described
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