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• W2103166599 abstract "The physical foundations of unsteady thin-airfoil theory are explored in the general framework of viscous flows. The thin-airfoil lift formula is derived by using the simple lift formula that contains the vortex lift and the lift associated with the fluid acceleration. From a broader perspective, the thin-airfoil lift formula could be applicable even when the flow around an airfoil is moderately separated, from which the classical von Kármán–Sears lift formula can be recovered as a reduced case. The quantitative relationship between boundary layer and lift generation is discussed. Direct numerical simulations of low-Reynolds-number flows over a flapping flat-plate airfoil are conducted to examine the accuracy and limitations of the thin-airfoil lift formula." @default.
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• W2103166599 date "2015-06-01" @default.
• W2103166599 modified "2023-09-30" @default.
• W2103166599 title "Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula" @default.
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• W2103166599 doi "https://doi.org/10.2514/1.j053439" @default.
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