Experimental determination of aerodynamic characteristics of an aircraft carrier at the stages of separation booster
Describes how to determine the aerodynamic characteristics ofaircraft carrierin the process of separation of bulkygoods, taking into account the interference interaction of the cargo and the carrierat lowsubsonicspeeds. Studies conducted by thegrid. The techniqueand developedan experimental setupto determine the aerodynamic characteristics of an aircraftcarrierat the stagesof separation fromitslaunch vehicle. Experimentally investigatedthe aerodynamic characteristics of the "aircraft carrier -rocket carrier". We obtain the aerodynamic characteristics of the aircraft carrier mounted with the bottomsurface of the load (RC) and the influence on the aerodynamic characteristics of the aircraft carrier. Investigatedbearingproperties, characteristics and resistance characteristics of theisolatedlongitudinal moment the aircraft carrierand cargo (RC).