Geometrically Nonlinear Random Response of Stiffened Laminated Plates by Proper-Orthogonal-Decomposition-Based Reduced-Order Modeling-Reference-Cited by-同舟云学术

Geometrically Nonlinear Random Response of Stiffened Laminated Plates by Proper-Orthogonal-Decomposition-Based Reduced-Order Modeling

Published:2021-11-11 Issue: Volume: Page:1-12
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Yang Shaochong¹,Yao Yuan¹,Li Youchen¹,Ma Lianhua¹,Zhang Ying¹,Yang Qingsheng²

Affiliation:

1. Hebei University, 071002 Baoding, People’s Republic of China

2. Beijing University of Technology, 100124 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Science and Technology Project of Hebei Education Department

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061095

Reference28 articles.

1. NemethM. P. “A Treatise on Equivalent-Plate Stiffnesses for Stiffened Laminated-Composite Plates and Plate-Like Lattices,” NASA Langley Research Center, NASA TP-2011-216882, Hampton, VA, 2011.

2. Vibration and stability analysis of stiffened plates by semi-analytic finite difference method, Part I: Consideration of bending displacements only

3. Free vibration of stiffened circular bridge decks

4. Vibration studies on some integral rib-stiffened plates

5. Computational study of strengthening effects of stiffeners on regular and arbitrarily stiffened plates

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