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 explain
β¦ LIBER β¦
Airfoil flow instabilities induced by background flow oscillations
β Scribed by W. C. Selerowicz; A. P. Szumowski
- Publisher
- Springer
- Year
- 2002
- Tongue
- English
- Weight
- 270 KB
- Volume
- 32
- Category
- Article
- ISSN
- 0723-4864
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