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Sandwich-Plate Vibration Analysis: Three-Layer Quasi-Three-Dimensional Finite Element Model

  • Published:2003-08 Issue:8 Volume:41 Page:1547-1555
  • ISSN:0001-1452
  • Container-title:AIAA Journal
  • language:en
  • Short-container-title:AIAA Journal

Author:

Nabarrete Airton1,de Almeida Sergio Frascino M.2,Hansen Jorn S.3

Affiliation:

1. Centro Universitario Fundacao Educacional Inaciana Pe Saboia de Medeiros, 09850-901 Sao Bernardo do Campo, Brazil

2. Instituto Tecnologico de Aeronautica, 12228-900 Sao Jose dos Campos, Brazil

3. University of Toronto, Toronto, Ontario M3H 5T6, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 27 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Layer-wise solutions for variable stiffness composite laminated sandwich plate using curvilinear fibers;Mechanics of Advanced Materials and Structures;2021-07-23

2. An efficient eight‐node quadrilateral element for free vibration analysis of multilayer sandwich plates;International Journal for Numerical Methods in Engineering;2021-02-11

3. A Three-Layer Quasi-3D Finite Element Analysis for Smart Actuation on Sandwich Plates;Journal of Vibration Engineering & Technologies;2020-11-18

4. Nonlinear Vibration Analysis of a Sandwich Beam and Assessment of the Dynamic Behavior;New Trends in Nonlinear Dynamics;2020

5. Soft-core sandwich plate dynamics: Theory and blast analysis;Journal of Sandwich Structures & Materials;2019-04-06
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