Flow field analysis of a 3D wing with flap based on N-S solution

DOI10.1007/BF01183682zbMath0989.76055OpenAlexW2020680526MaRDI QIDQ5943975

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Publication date: 22 July 2002

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

Full work available at URL: https://doi.org/10.1007/bf01183682

zbMATH Keywords

Navier-Stokes equationsartificial viscosityfinite volume methoddomain decompositiontime integrationcentral difference schemeconservation of fluxleading edge separated flowpatched gridside-edge region flowthree-dimensional wing with flap deflection

Mathematics Subject Classification ID

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

Related Items (2)

Comparative study of recent metaheuristics for solving a multiobjective transonic aeroelastic optimization of a composite wing ⋮ Comparison of predicting drag methods using computational fluid dynamics in 2d/3d viscous flow

Cites Work

• Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow

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