A study of non-oscillatory schemes based on LED principle for inviscid flow computation past airfoils

DOI10.1007/BF01170183zbMath0969.76053OpenAlexW2006722206MaRDI QIDQ1570851

N. Delaunay

Publication date: 1 October 2001

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01170183

zbMATH Keywords

finite volume schemesflux limitersEuler equationsshock wavesnonlinear scalar conservation lawscharacteristic decompositionswitching functionconvective upwind and split pressure techniquehigh resolution non-oscillatory discretization schemesinviscid transonic flow past airfoilslocal extremum diminishing principlescalar splittingsymmetric limited positive schemeupstream symmetric limited positive schemewave-particle splitting

Mathematics Subject Classification ID

Transonic flows (76H05) Finite volume methods applied to problems in fluid mechanics (76M12)

Related Items (1)

Evaluation of non-oscillatory schemes based on LED principle for supersonic flow computations

Uses Software

• SHASTA

Cites Work

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• High resolution schemes for hyperbolic conservation laws
• Construction of explicit and implicit symmetric TVD schemes and their applications
• Approximate Riemann solvers, parameter vectors, and difference schemes
• On central-difference and upwind schemes
• Computational algorithms for aerodynamic analysis and design
• Towards the ultimate conservative difference scheme. II: Monotonicity and conservation combined in a second-order scheme
• Riemann Solvers, the Entropy Condition, and Difference
• Flux-corrected transport. I: SHASTA, a fluid transport algorithm that works

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