Solution of the Euler equations for transonic flow over a lifting aerofoil - The Bernoulli formulation (Roe/Lytton method)
type: Item
instance of: scholarly article
title: Solution of the Euler equations for transonic flow over a lifting aerofoil - The Bernoulli formulation (Roe/Lytton method)
zbMATH Open document ID: 0633.76057
DOI: 10.1016/0021-9991(87)90144-6
author: C. C. Lytton
published in: Journal of Computational Physics
publication date: 1987-01-01T00:00:00Z
review text: The author's method, updated from that of Sells, for solving the Euler equations governing steady inviscid supercritical flow past an aerofoil, is described. Roe's ``Superbee'' algorithm is incorporated into an explicit flux-difference-splitting, non-time-split sequence of one- dimensional spatial operators in local-timestep mode. Results are presented for a parametric study of one supercritical case, as a check on the consistency of the method. The ability of the method to compute the flow over a bump on a channel wall is demonstrated. Results from the computation of a supercritical flow with recirculation are also shown.
Mathematics Subject Classification ID: 76H05
Mathematics Subject Classification ID: 76M99
zbMATH DE Number: 4031265
zbMATH Keywords: Euler equations
zbMATH Keywords: steady inviscid supercritical flow
zbMATH Keywords: ``Superbee'' algorithm
zbMATH Keywords: explicit flux-difference-splitting, non-time-split sequence of one-dimensional spatial operators
zbMATH Keywords: local-timestep mode
MaRDI profile type: Publication
full work available at URL: 0021-9991(87)90144-6
OpenAlex ID: W2012586614
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description: scientific article; zbMATH DE number 4031265