Implementation of an iterative algorithm for the coupled heat transfer in case of high-speed flow around a body

The results of investigation of a numerical technique for coupled heat transfer problem solving for an atmospheric supersonic flying vehicle and flow around it are presented. An iterative numerical algorithm and software package are developed for heat transfer simulation in a flying vehicle structure during its motion in the atmosphere. The convergence of variants of the iterative process for solution matching on the surface with ideal thermal contact is studied. The results of the numerical experiment confirm the obtained theoretical estimates.