Journal
AIAA JOURNAL
Volume 55, Issue 9, Pages 3143-3152Publisher
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J055763
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Funding
- National Basic Research Program of China [2014CB049000]
- National Natural Science Foundation of China [11372062, 11402049]
- China Postdoctoral Science Foundation [2015T80246]
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For the structural dynamic analysis of complicated beam-type structures, a detailed finite element model with large number of degrees of freedom is almost impossible to be used due to the huge computational cost and storage requirements. Therefore, a novel reduced-order model is proposed to determine the natural frequencies of the beam-type structures in this study, which is established by using a reduction basis along with the polynomial interpolation function. The basic idea is to convert the displacements of finite element model nodes in each cross section to a small set of nodes with a few generalized degrees of freedom. The proposed reduced-order model can gain a significant reduction of computational cost without sacrifice of accuracy; moreover, it has the ability to identify shell lobe-type modes and coupled modes. Several numerical case studies for different beam-type structures, including thin-walled cylinder, stiffened shells, and thin-walled cylinder with cutouts, are studied, and the outcomes are validated by benchmark studies.
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