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https://scholarbank.nus.edu.sg/handle/10635/111644
| Title: | Subsonic flow over unstalled pitching airfoil computed by Euler method | Authors: | Yang, S. Luo, S. Liu, F. Tsai, H.-M. |
Issue Date: | 2006 | Citation: | Yang, S.,Luo, S.,Liu, F.,Tsai, H.-M. (2006). Subsonic flow over unstalled pitching airfoil computed by Euler method. Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference 4 : 2744-2759. ScholarBank@NUS Repository. | Abstract: | Subsonic flow about a sinusoidally pitching airfoil with mean angle of attack is studied by an unsteady compressible Euler now solver. Fully attached flows are considered. The Euler method is evaluated extensively by wind-tunnel test data of two no-stall cases for pitching-oscillating airfoil NACA 0012 in the literature. The wind tunnel walls are not considered in the computations. The boundary layer effects are identified. The effects of mean angle of attack on the fluctuating forces are studied. | Source Title: | Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference | URI: | http://scholarbank.nus.edu.sg/handle/10635/111644 | ISBN: | 1563478102 |
| Appears in Collections: | Staff Publications |
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