Aerodynamic simulation using compact upwind schemes on unstructured grids

摘要

The progress on monotone shock capturing matrix distribution schemes for unstructured grids, first introduced at the ECCOMAS96 conference, is reviewed. Since then, the schemes have been applied in three space dimensions on hypersonic and transonic configurations and the extension to viscous flows has been made; parallelized implicit time integration has been added as well as two-equation turbulence modeling for Reynolds averaged Navier-Stokes simulation. Numerical simulations for a transonic wing and for a turbulent shock wave boundary layer interaction show that the method can be used for industrial application.