Abstract—
This work is devoted to the numerical study of the thermal regime of the retort surface in an apparatus for the production of titanium. The problem of conjugate heat transfer between the wall of a cylindrical retort and the wall of a furnace with heaters is considered. There is a gap with forced air flow between the walls. The purpose of this study is to estimate temperature conditions of the retort wall and the heat transfer coefficient on its surface under various heating or cooling conditions occurring in the apparatus. Data on the distribution of heat fluxes on the retort walls are required for the calculation of turbulent convective flows of liquid magnesium inside the retort, since temperature nonuniformity can have a strong effect on the processes occurring inside it. The computational domain consists of solid walls and an air flow between them. The mathematical model is based on a system of axially symmetric nonstationary Navier–Stokes equations, and the RANS (Reynolds-averaged Navier–Stokes equations) approach is used to describe turbulent fields. In addition to heat transfer by forced convection and thermal conductivity, the model also considers the radiation heat transfer between two opposite walls. Four heating options, which can be used during operation of the reactor, are investigated. The air flow velocity required to keep the retort wall temperature in the allowable working range from 750 to 950°C under all operating conditions, was estimated. The temperature distribution along the investigated segment of the retort wall is demonstrated to be nonuniform. Dependencies for the heat transfer coefficient at the side surface of the retort on the vertical coordinate were constructed. The predictions by these dependencies were compared with the known formula for the heat transfer coefficient on a plane infinite surface with a constant heat flux. It has been established that in this case, which is more intricate, the calculated coefficients are close to those predicted by the known engineering formulas only for a part of the regimes examined in this study. Noticeable differences between the obtained dependencies and simplified estimations were found in a wide range of the studied parameters. The largest difference is observed at the channel inlet where the temperature gradients are maximal.
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Karasev, T.O., Teimurazov, A.S. & Perminov, A.V. Numerical Study of Heat Transfer from an Air-Cooled Wall of a Titanium Reactor. J Appl Mech Tech Phy 62, 1243–1254 (2021). https://doi.org/10.1134/S0021894421070117
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DOI: https://doi.org/10.1134/S0021894421070117