Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil
Kryštůfek P., Kozel K.
EPJ Web of Conferences · 2014
doi:10.1051/epjconf/20146702061 (opens in a new tab)
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Abstract
The article presents results of a numerical solution of subsonic, transonic and supersonic flows described by the system of Navier-Stokes equations in 2D laminar compressible flows around the RAE 2822 airfoil. Authors used FVM multistage Runge-Kutta method to numerically solve the flows around the RAE 2822 airfoil.
Abstract licence: CC BY
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