Abstract
In this paper, the results of analysis of the high speed gas flow over a sphere are presented. Numerical investigations were carried out using the UST3D code developed at the Ishlinsky Institute for Problems in Mechanics of RAS (IPMech RAS). The code implements numerical simulation of aerothermodynamics of aircrafts in the context of integration of the full system of Navier – Stokes equations on unstructured mesh using the perfect gas model.
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