Numerical Calculation of the Viscid Gas Flow in the Vicinity of a Multi-Stage Launcher with the On-Caliber Fairing
Obtained results using average Reynolds-Navier-Stokes equations of the mathematical modeling of the viscid gas flow in the vicinity of a multi-stage launcher with the on-caliber fairing at subsonic, transonic and supersonic speeds are presented. Stationary distributed aerodynamic loadings are examined. Receipted flow pictures are described. A comparison of calculated and experimental data is carried out.