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Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow

✍ Scribed by Tang, Deman; Dowell, Earl H.; Hall, Kenneth C.


Book ID
126317802
Publisher
American Institute of Aeronautics and Astronautics
Year
1999
Tongue
English
Weight
433 KB
Volume
37
Category
Article
ISSN
0001-1452

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A low-dimensional model for the planar nonlinear dynamics of a fluid-conveying cantilever is constructed using the proper orthogonal decomposition method (PODM) in the post-flutter region. Firstly, the nonlinear partial differential equation (PDE) of motion is converted into a finite set of coupled