The Euler and Navier-Stokes solutions of a 3-D wing with aileron

DOI10.1007/BF01179541zbMath0945.76051OpenAlexW1999814926MaRDI QIDQ1818650

Yanyan Li

Publication date: 4 January 2000

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

Full work available at URL: https://doi.org/10.1007/bf01179541

zbMATH Keywords

Navier-Stokes equationsEuler equationsfinite volume discretizationconservation of fluxtime marchingdomain decomposition techniqueflux vector splitting schemecentral difference schemesinternal boundary conditionlimiter functionpatched gridsvan Leer's schemewings with control surfaces

Mathematics Subject Classification ID

Transonic flows (76H05) Finite volume methods applied to problems in fluid mechanics (76M12) Gas dynamics (general theory) (76N15)

Related Items (1)

Comparative study of recent metaheuristics for solving a multiobjective transonic aeroelastic optimization of a composite wing

Cites Work

• Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
• Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow

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