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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| Main Authors: | , , |
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| Format: | article |
| Language: | EN |
| Published: |
Isfahan University of Technology
2021
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| Subjects: | |
| Online Access: | https://doaj.org/article/da2abd98485a40b185207da87a7ad7fd |
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