Stabilized methods for high-speed compressible flows: toward hypersonic simulations

نویسندگان

چکیده

A stabilized finite element framework for high-speed compressible flows is presented. The Streamline-Upwind/Petrov–Galerkin formulation augmented with discontinuity-capturing (DC) are the main constituents of that enable accurate, efficient, and stable simulations in this flow regime. Full- reduced-energy formulations employed class problems their relative accuracy assessed. In addition, a recently developed DC presented shown to be particularly well suited hypersonic flows. Several verification validation cases, ranging from 1D 3D supersonic regimes, show excellent performance proposed set stage its deployment on more advanced applications.

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ژورنال

عنوان ژورنال: Computational Mechanics

سال: 2021

ISSN: ['0178-7675', '1432-0924']

DOI: https://doi.org/10.1007/s00466-020-01963-6