Free vibration of two-layered cross-ply laminated plates using layer-wise trigonometric shear deformation theory

被引:6
作者
Shimpi, RP [1 ]
Ainapure, AV [1 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Bombay 400076, Maharashtra, India
关键词
free vibration; shear deformation; rotary inertia; layer-wise theory; laminated thick plate; cross-ply plate;
D O I
10.1177/0731684404031893
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this paper, variationally consistent layer-wise trigonometric shear deformation theory has been extended to deal with free vibration of two-layered laminated cross-ply plates. Governing differential equations are derived by making use of a displacement field which allows a sinusoidal variation of the in-plane displacements through the laminate thickness. In this displacement based theory, constitutive relations between shear-stress and shear-strains are satisfied in both the layers, and, therefore, shear correction factor is not required. Compatibility at the layer interface in respect of in-plane displacement and compatibility in respect of transverse shear-stress is satisfied, yet present theory contains fewer unknown variables than that of the first order shear deformation theory. Effects of rotary inertia and other inertias are also included. Efficacy of the present theory is demonstrated through illustrative examples.
引用
收藏
页码:389 / 405
页数:17
相关论文
共 50 条
  • [31] Buckling and free vibration analyses of laminated composite plates by using two new hyperbolic shear-deformation theories
    S. S. Akavci
    A. H. Tanrikulu
    Mechanics of Composite Materials, 2008, 44
  • [32] Buckling and free vibration analyses of laminated composite plates by using two new hyperbolic shear-deformation theories
    Akavci, S. S.
    Tanrikulu, A. H.
    MECHANICS OF COMPOSITE MATERIALS, 2008, 44 (02) : 145 - 154
  • [33] Free vibration and buckling analysis of cross-ply laminated composite plates using Carrera's unified formulation based on Isogeometric approach
    Alesadi, Amirhadi
    Galehdari, Marzieh
    Shojaee, Saeed
    COMPUTERS & STRUCTURES, 2017, 183 : 38 - 47
  • [34] A Comparison of Closed-Form and Finite-Element Solutions for the Free Vibration of Hybrid Cross-Ply Laminated Plates
    M. A. Benhenni
    B. Adim
    T. Hassaine Daouadji
    B. Abbès
    F. Abbès
    Y. Li
    A. Bouzidane
    Mechanics of Composite Materials, 2019, 55 : 181 - 194
  • [35] A Comparison of Closed-Form and Finite-Element Solutions for the Free Vibration of Hybrid Cross-Ply Laminated Plates
    Benhenni, M. A.
    Adim, B.
    Daouadji, T. Hassaine
    Abbes, B.
    Abbes, F.
    Li, Y.
    Bouzidane, A.
    MECHANICS OF COMPOSITE MATERIALS, 2019, 55 (02) : 181 - 194
  • [36] Effects of in-plane loads on free vibration of symmetrically cross-ply laminated plates resting on Pasternak foundation and coupled with fluid
    Shahbaztabar, Arash
    Ranji, Ahmad Rahbar
    OCEAN ENGINEERING, 2016, 115 : 196 - 209
  • [37] A new trigonometric shear deformation plate theory for free vibration analysis of FGM plates with two-directional variable thickness
    Hoang, Vu Ngoc Viet
    Thanh, Pham Trung
    THIN-WALLED STRUCTURES, 2024, 194
  • [38] Analysis of Thick Rectangular Plates with Symmetric Cross-ply Laminates Based on First-order Shear Deformation Theory
    Civalek, Oemer
    JOURNAL OF COMPOSITE MATERIALS, 2008, 42 (26) : 2853 - 2867
  • [39] 3D free vibration analysis of cross-ply laminated plates with one pair of opposite edges simply supported
    Chen, WQ
    Lüe, CF
    COMPOSITE STRUCTURES, 2005, 69 (01) : 77 - 87
  • [40] Buckling and free vibration analysis of laminated composite plates using an efficient and simple higher order shear deformation theory
    Adim, Belkacem
    Daouadji, Tahar Hassaine
    Abbes, Boussad
    Rabahi, A.
    MECHANICS & INDUSTRY, 2016, 17 (05)