Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles

The article discusses the flow features of canard-controlled missiles with account to aerodynamic cross- connections conditioned upon the interaction of the spectra of the flow around the canard, tail and body. The results of a numerical analysis of the influence of the relative position of the canard and tail on the integrated aerodynamic characteristics are shown. The possibility of controlling the flow by reducing the intensity of the end vortex generated by the canard is shown.