Abstract: | The contribution presents several results achieved by central and upwind type schemes for some internal and external flow problems in 2D and 3D. Results of transonic flow through cascade shows the behavior of methods and influence of different implementation of boundary conditions. Numerical solution of 2D external flow problems based on inviscid flow ‐ boundary layer interaction method has been used for wind tunnel wall correction. Presented results show improvement of correction method in region of transonic flow. |