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- W2315474418 abstract "The unsteady separated turbulent flow around an oscillating airfoil plunging in a sinusoidal pattern in the regime of low Reynolds number is investigated numerically, employing the URANS approach with advanced turbulence model, k-SST transitional. A comparison with experimental data shows that the Transition SST model is capable of predicting the flow characteristics for the increasing cycle while the main difficulty lies in the accurate modeling of the complicated separated flows during the decreasing stroke. The flow development of the dynamic stall is also discussed." @default.
- W2315474418 created "2016-06-24" @default.
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- W2315474418 date "2011-05-31" @default.
- W2315474418 modified "2023-09-27" @default.
- W2315474418 title "Numerical investigation of dynamic stall phenomenon on a plunging airfoil" @default.
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- W2315474418 doi "https://doi.org/10.2495/cmem110061" @default.
- W2315474418 hasPublicationYear "2011" @default.
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