Investigation of the Influence of Pressure Redistribution Arising Out of the Cross Flow Jet to the Aerodynamic Characteristics of the Axisimmetric Supersonic Vehicle.

The effect blowing out of combustion products for the aerodynamic characteristics of an axisymmetric body in a supersonic flow is considered. The flow patterns are obtained, using the Schlieren method, in the case without blowing and blowing the jet. Also, the results of the force loads acting on the model in the experiment, using strain gauges, were obtained. The investigations were carried out for the case of flow past a zero angle of attack α = 0 ° and with Mach number M = 4 in the wind tunnel "Transit-M". [ABSTRACT FROM AUTHOR]