Article ID Journal Published Year Pages File Type
7154241 Chinese Journal of Aeronautics 2016 10 Pages PDF
Abstract
This paper deals with the numerical solution of inviscid compressible flows. The three-dimensional Euler equations describing the mentioned problem are presented and solved numerically with the finite volume method. The evaluation of the numerical flux at the interfaces is performed by using the Toro Vazquez-Harten Lax Leer (TV-HLL) scheme. An essential feature of the proposed scheme is to associate two systems of differential equations, called the advection system and the pressure system. It can be implemented with a very simple manner in the standard finite volume Euler and Navier-Stokes codes as extremely simple task. The scheme is applied to some test problems covering a wide spectrum of Mach numbers, including hypersonic, low speed flow and three-dimensional aerodynamics applications.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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