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Implementation of an iterative algorithm for the coupled heat transfer in case of high-speed flow around a body. (English) Zbl 1410.76172
Summary: Results of an investigation of a numerical technique for the coupled heat transfer problem solved 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. Results of the numerical experiment confirm the obtained theoretical estimates.
76M10 Finite element methods applied to problems in fluid mechanics
65M60 Finite element, Rayleigh-Ritz and Galerkin methods for initial value and initial-boundary value problems involving PDEs
65Y15 Packaged methods for numerical algorithms
76-04 Software, source code, etc. for problems pertaining to fluid mechanics
76J20 Supersonic flows
76N15 Gas dynamics, general
76V05 Reaction effects in flows
76L05 Shock waves and blast waves in fluid mechanics
Full Text: DOI
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