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Flux-difference split algorithm for unsteady thin-layer Navier-Stokes solutions

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Publication:3992397
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DOI10.2514/3.11009zbMath0756.76054OpenAlexW1967598374MaRDI QIDQ3992397

David L. Whitfield, L. Bruce Simpson

Publication date: 13 August 1992

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.11009

zbMATH Keywords

oscillating airfoilsdiffusive termsflat plate laminar boundary-layer profileNewton subiteration techniquethree grid cells


Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)


Related Items

Flow field saddles and their relation to vortex asymmetry, A parallelized ENO procedure for direct numerical simulation of compressible turbulence, High-resolution viscous flow simulations at arbitrary Mach number.



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