Abstract
The effect of the turbulence intensity of the oncoming stream on the aerodynamic characteristics of the NACA-0012 airfoil is investigated by a direct numerical simulation. The numerical results are found to be consistent with the experimental measurements. Based on the finite spectral QUICK scheme, the simulation gets the high accuracy results. Both the simulation and the experiment reveal that the airfoil stall does not exist for the low turbulence intensity, however, occurs when the turbulence intensity increases sufficiently. Besides, the turbulence intensity has a significant effect on both the airfoil boundary layer and the separated shear layer.
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Communicated by Wen-rui HU
Project supported by the National Natural Science Foundation of China (No. 108720006) and the National Basic Research Program of China (973 Program) (No. 2007CB714601)
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Li, Sw., Wang, S., Wang, Jp. et al. Effect of turbulence intensity on airfoil flow: numerical simulations and experimental measurements. Appl. Math. Mech.-Engl. Ed. 32, 1029–1038 (2011). https://doi.org/10.1007/s10483-011-1478-8
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DOI: https://doi.org/10.1007/s10483-011-1478-8
Key words
- finite spectral method
- turbulence intensity
- boundary layer
- shear layer
- lift force
- drag force
- airfoil stall