To Determine the Distribution of Monobloc Layouts Aerodynamic Characteristics
The determination and analysis of monoblock layouts aerodynamic characteristics that are necessary for determining the load on the body of promising launchers are given. As launchers configurations were investigated a cylinder-conical shape body with the presence of superstructures, fairings and aerodynamic rudders at the aft are noted. A numerical modeling of a flow in the framework of Euler equations describing the flow of an inviscid gas, and within Navier - Stokes equations describing the flow of a viscous gas were carried out. A comparison of the results of the experimental and numerical simulation of distributed aerodynamic characteristics, showing their good agreement were carried out.