Upwind formulations for the Euler equations in steady supersonic flows
Author:
Affiliation:
1. Politecnico di Torino, Torino, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10111
Reference14 articles.
1. A locally two-dimensional numerical method for calculating three-dimensional supersonic flows
2. The λ-scheme
3. The Split Coefficient Matrix method for hyperbolic systems of gasdynamic equations
4. Approximate Riemann solvers, parameter vectors, and difference schemes
5. Computation of steady supersonic flows by a flux-difference/splitting method
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1. Discontinuities in Compressible Flows: Italian Contributions;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2009
2. A higher-order Godunov method for the hyperbolic equations modelling shock dynamics;Proceedings of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences;1999-04-08
3. Hyperbolicity and Optimal Coordinates for the Three-Dimensional Supersonic Euler Equations;SIAM Journal on Applied Mathematics;1997-08
4. A split-matrix runge-kutta type space marching procedure;Journal of Computational Physics;1992-10
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