To a problem of a stability improvement of axisymmetric bodies in the range of supersonic speeds

The stability improvement problem of axisymmetric bodies at the range of supersonic speeds is considered. For improving moment characteristics the deflected nose and four movable flaps were used. Researches were conducted in the range of Mach numbers M = 3.10 and angles of attack α = 1.30°. The improving capability of the moment characteristics of the body is achieved. Special feature of interference of the deflected nose and movable flaps to aerodynamic characteristics were considerd.