Simulation of supersonic flows on the basis of splitting algorithms
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DOI: 10.1134/s0021894417050054
Abstract: For the numerical simulation of aerodynamics problems, the Euler and Navier — Stokes equations written in integral form are used to construct an implicit finite-volume predictor-corrector scheme. At the predictor stage, the splitting of equations… read more here.
Keywords: supersonic flows; splitting algorithms; flows basis; basis splitting ... See more keywords