Experimental Research and Calculation of Parameters of Hypersonic Separated Flow Around Aerodynamic Flaps Under Their Interference

Various combinations of aft body flaps have been examined to determine the effectiveness of control of flow around cone-shaped bodies. Possible structures of flow around controls and their transformation depending on construction and gasdynamic parameters have been revealed. The applicable mathematical model is developed and parametric calculations are conducted to determine aerodynamic characteristics of such bodies with flaps under the hypersonic flow conditions.