The Study Of Aerodynamic Characteristics Of Afterbody And Effect Of Cable-Mounting
机身后体气动特性及其张线支撑影响研究

The purpose of this paper is to study the effect of cable-mounting on flow over an afterbody of a aircraft. The experimental results show that: (1) the flow patterns over afterbody can be divided into upper-separated, non-separated and under-separated type; (2) the cable influences the aerodynamic characteristics of the model by affecting the vortex structure over it; (3) the basic flow patterns over afterbody have not been changed evidently by any of these three types of cable-mounting configuration.