Numerical Simulation of Limit-cycle Oscillations of a Cropped Delta Wing Using the Full Navier-Stokes Equations

DOI10.1080/10618560108940725zbMath1058.76044OpenAlexW2071478208MaRDI QIDQ2744475

Raymond E. Gordnier, Reid B. Melville

Publication date: 2001

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618560108940725

zbMATH Keywords

Euler equationsleading-edge vortexdouble shock structureimplicit approximately-factored finite difference Beam-Warming algorithm

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Gas dynamics (general theory) (76N15)

Related Items (1)

Flutter prediction by an Euler method on non-moving Cartesian grids with gridless boundary conditions

Cites Work

• A diagonal form of an implicit approximate-factorization algorithm
• Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow
• Geometric Conservation Law and Its Application to Flow Computations on Moving Grids
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations

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