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- W2334797480 abstract "Results are presented from an experimental study of stall flutter oscillations from a twodegree-of-freedom, pitch/plunge airfoil system with nonlinear structural stiffness in the plunge direction. With linear (only) structural stiffness, the airfoil system could exhibit a large-pitch-amplitude limit cycle response which is attributed to stall. With the addition of the nonlinear stiffness, the airfoil system could exhibit two classes of limit cycle response: one with low-pitch-amplitude attributed to the structural nonlinearity and one with highpitch-amplitude attributed to stall. The amplitudes of the limit cycles for cases in which the structural and aerodynamic nonlinearities co-exist are modulated and remain steady over a range of airspeeds and for initial excitations above a critical value." @default.
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- W2334797480 date "2013-04-05" @default.
- W2334797480 modified "2023-10-16" @default.
- W2334797480 title "Stall Flutter Oscillation Measurements from a Two Degree-of-Freedom Airfoil with Nonlinear Stiffness" @default.
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- W2334797480 doi "https://doi.org/10.2514/6.2013-1842" @default.
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