TY - GEN
T1 - Large-eddy simulation of the flow over a thin airfoil at low reynolds number
AU - Kojima, Ryoji
AU - Nonomura, Taku
AU - Oyama, Akira
AU - Fujii, Kozo
N1 - Copyright:
Copyright 2021 Elsevier B.V., All rights reserved.
PY - 2011
Y1 - 2011
N2 - 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.
AB - 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.
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U2 - 10.1007/978-3-642-17884-9_116
DO - 10.1007/978-3-642-17884-9_116
M3 - Conference contribution
AN - SCOPUS:84890280110
SN - 9783642178832
T3 - Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010
SP - 885
EP - 886
BT - Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010
PB - Kluwer Academic Publishers
T2 - 6th International Conference on Computational Fluid Dynamics, ICCFD 2010
Y2 - 12 July 2010 through 16 July 2010
ER -