Numerical modeling of thermophysical processes in the air cooling channel of the titanium sponge reduction reactor is performed. The cooling channel is an area bounded by a retort filled with liquid magnesium and a wall on which heating elements are mounted. Air flows inside the channel, cooling the retort. A mathematical model is constructed based on unsteady Navier-Stokes equations in axisymmetric formulation using a k −ω SST turbulence model. The model takes into account the radiation heat transfer between the retort and reactor walls. Two variants of thermal boundary conditions are considered. The temperature conditions of the retort wall have been calculated, and the profiles of the heat transfer coefficient along the retort wall for a wide interval of airflow rates have been obtained. It is shown that temperature distributions along the retort are not uniform and strongly depend both on external boundary conditions and on cooling intensity. Heat transfer coefficient distributions from its outer wall for different retort heating conditions are plotted, and an empirical formula for calculating the profile of this coefficient is proposed.