Aeroelastic Simulation of Stall Flutter Undergoing High ‎and Low Amplitude Limit Cycle Oscillations

The aeroelastic behaviour of an airfoil oscillating in large and small pitch amplitudes due to nonlinearity ‎in aerodynamics is examined. The phenomenon of stall flutter resulted in the limit cycle oscillations of ‎NACA 0012 at low to intermediate Reynolds number is investigated numerically through...

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Autores principales: M. K. H. M. Zorkipli, A. Abbas, N. A. Razak
Formato: article
Lenguaje:EN
Publicado: Isfahan University of Technology 2021
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Acceso en línea:https://doaj.org/article/da2abd98485a40b185207da87a7ad7fd
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