Numerical Solution of Inviscid Compressible Steady Flows around the RAE 2822 Airfoil
The article presents results of a numerical solution of subsonic, transonic and supersonic flows described by the system of Euler equations in 2D compressible flows around the RAE 2822 airfoil. Authors used FVM multistage Runge-Kutta method to numerically solve the flows around the RAE 2822 airfoil....
Main Authors: | Kryštůfek P., Kozel K. |
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Format: | Article |
Language: | English |
Published: |
EDP Sciences
2015-01-01
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Series: | EPJ Web of Conferences |
Online Access: | http://dx.doi.org/10.1051/epjconf/20159202041 |
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