Characteristic-Based Flux Splitting to Solve Compressible Flow over an Airfoil
نویسندگان
چکیده
منابع مشابه
Instabilities of Stationary Inviscid Compressible Flow around an Airfoil
In this paper we numerically solve the stationary inviscid flow around an airfoil. Using the second-order explicit Runge–Kutta method in combination with the MUSCL scheme and the minmod limiter, we do not obtain a machine accurate solution. This has already been observed in literature and is explained by the non-differentiability of the minmod limiter. An analysis of the limiter shows that it i...
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ژورنال
عنوان ژورنال: Mapta Journal of Mechanical and Industrial Engineering (MJMIE)
سال: 2018
ISSN: 2517-4258
DOI: 10.33544/mjmie.v2i3.80