The objective of this investigation is to evaluate the transient effects of a reaction control jet on the aerodynamic performance of a generic interceptor missi
Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flowfield around a generic canard-controlled missile confi
Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flowfield around a generic canard-controlled missile confi
A detailed numerical investigation of the interaction between a lateral jet and the external flow has been performed for a variety of missile body geometries. T