Organised modes and shock--vortex interaction in unsteady viscous transonic flows around an aerofoil. I: Mach number effect.
type: Item
instance of: scholarly article
title: Organised modes and shock--vortex interaction in unsteady viscous transonic flows around an aerofoil. I: Mach number effect.
zbMATH Open document ID: 1039.76517
DOI: 10.1016/S0045-7930(02)00100-7
author: A. Bouhadji
author: M. Braza
published in: Computers and Fluids
publication date: 2003-12-09T00:00:00Z
Mathematics Subject Classification ID: 76H05
Mathematics Subject Classification ID: 76L05
zbMATH DE Number: 2015067
MaRDI profile type: Publication
cites work: Q3026940
cites work: Q3768576
cites work: On finite element approximation and stabilization methods for compressible viscous flows
cites work: Q3994419
cites work: Approximate Riemann solvers, parameter vectors, and difference schemes
cites work: Q3768578
cites work: Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries
cites work: Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
description: scientific article; zbMATH DE number 2015067