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Published in 2017 at "Journal of Applied Mechanics and Technical Physics"
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…
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Keywords:
supersonic flows;
splitting algorithms;
flows basis;
basis splitting ... See more keywords