Abstract:
The software package to calculate parameters of three-dimensional steady and unsteady gas flows in complex devices is presented. The mathematical flow model used in package is based on the Reynolds-averaged Navier Stokes equations for a two-component equilibrium turbulent medium and a two-parameter semiempirical turbulence model. A numerical implementation of the software package to modelling three complex flows in modern devices is described.
Citation:
V. N. Koterov, V. M. Krivtsov, V. I. Zubov, “Software package to calculate the aerodynamic characteristics of aircrafts”, Proceedings of ISP RAS, 29:6 (2017), 271–288