Three-dimensional supersonic flow analysis over a satellite vehicle launcher

DOI10.1016/S0377-0427(98)00238-6zbMath0962.76058OpenAlexW2092256249MaRDI QIDQ1300722

Álvaro Luiz De Bortoli

Publication date: 2 September 1999

Published in: Journal of Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0377-0427(98)00238-6

zbMATH Keywords

preconditioningsupersonic flowmultigridcompressible fluidalmost incompressible fluidcentral spatial discretizationfinite volume explicit Runge-Kutta multistage schemevehicle launcher

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Multigrid methods; domain decomposition for initial value and initial-boundary value problems involving PDEs (65M55) Supersonic flows (76J20)

Cites Work

• The application of preconditioning in viscous flows
• The MEGAFLOW Project — Numerical Flow Simulation for Aircraft
• Unnamed Item

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