Computational modeling for three-dimensional viscous sub/supersonic flows with shock waves

The description of computational method is submitted for three-dimensional viscous flows with shock waves. The description of the Boldwin-Lomax algorithm of turbulent viscous calculation is stated. On the base of presented method a set of 3-D flows in channels and engine nozzles and some classical problems are computed. Calculation results are compared with experimental data for local and integral parameters.