Abstract
Mechanisms of quasi-periodic flow oscillation observed in airfoils near stall and stall behaviour, which affect airfoil efficiency, remain still not fully understood. In this sense, numerical simulations using subgrid-scale models can be useful in order to shed some light in the underlying complex physics. However, the assessment of these models is an important aspect to consider for obtaining credible results. In this work, two LES models are compared with results from direct numerical simulation. The results have shown that LES models are capable of capturing the complex flow phenomena present at these AOA such as the low frequency fluctuations near stall and the vortex shedding produced at higher AOAs.
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Rodríguez, I., Lehmkuhl, O., Baez, A., Perez-Segarra, C.D. (2014). On LES Assessment in Massive Separated Flows: Flow Past a NACA Airfoil at Re = 50000. In: Hölling, M., Peinke, J., Ivanell, S. (eds) Wind Energy - Impact of Turbulence. Research Topics in Wind Energy, vol 2. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-54696-9_24
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DOI: https://doi.org/10.1007/978-3-642-54696-9_24
Publisher Name: Springer, Berlin, Heidelberg
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