Efficiency of two approaches to computing the flow around an airfoil with flaps in the case of flow separation

DOI10.1134/S0965542519010044zbMath1453.76090OpenAlexW2945940136MaRDI QIDQ2314196

S. V. Matyash, M. F. Engulatova, V. V. Vlasenko, S. S. Molev, S. M. Bosnyakov, S. V. Mikhailov

Publication date: 19 July 2019

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0965542519010044

zbMATH Keywords

convergenceefficiencyexperimental datagridairfoilflapsfractional stepglobal stepdual step

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25) Finite volume methods for initial value and initial-boundary value problems involving PDEs (65M08)

Cites Work

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• Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge
• Adaptive mesh refinement -- theory and applications. Proceedings of the Chicago workshop on adaptive mesh refinement methods, Chicago, IL, USA, September 3--5, 2003.
• Adaptive mesh refinement for hyperbolic partial differential equations
• Approximate Riemann solvers, parameter vectors, and difference schemes
• Reassessment of the wall functions approach for RANS computations

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