Abstract
The performance of airfoil NACA0002 at Reynolds number of 2.3 × 104 is investigated with large-eddy simulation (LES). The angle of attack is 3, 6, or 9 degree. The behavior of a laminar separation bubble which appears over a thin airfoil and its effects on aerodynamic characteristics are mainly discussed. © 2011 Springer-Verlag Berlin Heidelberg.
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CITATION STYLE
Kojima, R., Nonomura, T., Oyama, A., & Fujii, K. (2011). Large-eddy simulation of the flow over a thin airfoil at low reynolds number. In Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010 (pp. 885–886). Kluwer Academic Publishers. https://doi.org/10.1007/978-3-642-17884-9_116
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