On the free vibration analysis of laminated composite and sandwich plates: A review of recent literature with some numerical results

The present article reviews the recent research done on the free vibration analysis of multilayered laminated composite and sandwich plates using various methods available for the analysis of plates. Displacement fields of various displacement based shear deformation theories have been presented and...

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Published inComposite structures Vol. 129; pp. 177 - 201
Main Authors Sayyad, Atteshamuddin S., Ghugal, Yuwaraj M.
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.10.2015
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Abstract The present article reviews the recent research done on the free vibration analysis of multilayered laminated composite and sandwich plates using various methods available for the analysis of plates. Displacement fields of various displacement based shear deformation theories have been presented and compared. Also, some numerical results related to fundamental flexural mode frequencies of laminated composite and sandwich plates are presented using a trigonometric shear and normal deformation theory. The theory involves six unknown variables and does not require problem dependent shear correction factor. Governing differential equations and associated boundary conditions of the theory are derived by employing the dynamic version of the principle of virtual work. Navier-type closed-form solutions are obtained for simply supported laminated composite and sandwich plates. The present results are compared with exact elasticity solution and other higher order shear deformation theories wherever applicable. This article cites 391 references.
AbstractList The present article reviews the recent research done on the free vibration analysis of multilayered laminated composite and sandwich plates using various methods available for the analysis of plates. Displacement fields of various displacement based shear deformation theories have been presented and compared. Also, some numerical results related to fundamental flexural mode frequencies of laminated composite and sandwich plates are presented using a trigonometric shear and normal deformation theory. The theory involves six unknown variables and does not require problem dependent shear correction factor. Governing differential equations and associated boundary conditions of the theory are derived by employing the dynamic version of the principle of virtual work. Navier-type closed-form solutions are obtained for simply supported laminated composite and sandwich plates. The present results are compared with exact elasticity solution and other higher order shear deformation theories wherever applicable. This article cites 391 references.
Author Sayyad, Atteshamuddin S.
Ghugal, Yuwaraj M.
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  surname: Sayyad
  fullname: Sayyad, Atteshamuddin S.
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  organization: Department of Civil Engineering, SRES’s College of Engineering, Savitribai Phule Pune University, Kopargaon 423601, Maharashtra, India
– sequence: 2
  givenname: Yuwaraj M.
  surname: Ghugal
  fullname: Ghugal, Yuwaraj M.
  organization: Department of Applied Mechanics, Government College of Engineering, Karad 415124, Maharashtra, India
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Snippet The present article reviews the recent research done on the free vibration analysis of multilayered laminated composite and sandwich plates using various...
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SubjectTerms Free vibration
Laminated composite
Natural frequency
Normal strain/stress
Sandwich plate
Shear deformation theory
Title On the free vibration analysis of laminated composite and sandwich plates: A review of recent literature with some numerical results
URI https://dx.doi.org/10.1016/j.compstruct.2015.04.007
Volume 129
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