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
β¦ LIBER β¦
Limit cycle oscillation of a fluttering cantilever plate
β Scribed by Weiliang, Ye ;Dowell, Earl
- Book ID
- 121338036
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1991
- Tongue
- English
- Weight
- 668 KB
- Volume
- 29
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.10821
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