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Development of a Three-Dimensional Unstructured Euler Solver for High-Speed Flows
English
2015
INCAS Bulletin
English
This paper addresses the solution of the compressible Euler equations on hexahedral meshes for supersonic and hypersonic flows. Spatial discretization is accomplished by a cell-centered finite-volume formulation which employs two different upwind schemes for the computation of convective fluxes. Second-order solutions are attained through a linear state reconstruction technique that yields highly resolved flows in smooth regions while providing a sharp and clean resolution of shocks. The
doi:10.13111/2066-8201.2015.7.4.1
fatcat:w4doegakqnad7mogttwifvcihq