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 32 条
[1]  
[Anonymous], ASCE P J ENG MECH DI
[2]   COMPOSITE-MATERIAL MECHANICS - STRUCTURAL MECHANICS [J].
BERT, CW ;
FRANCIS, PH .
AIAA JOURNAL, 1974, 12 (09) :1173-1186
[3]   FREE-VIBRATIONS OF LAMINATED RECTANGULAR-PLATES ANALYZED BY HIGHER-ORDER INDIVIDUAL-LAYER THEORY - COMMENT [J].
BHASKAR, K ;
VARADAN, TK .
JOURNAL OF SOUND AND VIBRATION, 1992, 154 (01) :178-179
[4]   Analysis of composite plates using various plate theories - Part 2: Finite element model and numerical results [J].
Bose, P ;
Reddy, JN .
STRUCTURAL ENGINEERING AND MECHANICS, 1998, 6 (07) :727-746
[5]   Analysis of composite plates using various plate theories Part 1. Formulation and analytical solutions [J].
Bose, P ;
Reddy, JN .
STRUCTURAL ENGINEERING AND MECHANICS, 1998, 6 (06) :583-612
[6]   FREE-VIBRATIONS OF LAMINATED RECTANGULAR-PLATES ANALYZED BY HIGHER-ORDER INDIVIDUAL-LAYER THEORY [J].
CHO, KN ;
BERT, CW ;
STRIZ, AG .
JOURNAL OF SOUND AND VIBRATION, 1991, 145 (03) :429-442
[7]   AN EFFICIENT HIGHER-ORDER PLATE-THEORY FOR LAMINATED COMPOSITES [J].
CHO, MH ;
PARMERTER, RR .
COMPOSITE STRUCTURES, 1992, 20 (02) :113-123
[8]  
DISCIUVA M, 1992, COMPOS STRUCT, V22, P149, DOI 10.1016/0263-8223(92)90003-U
[9]   A HIGHER-ORDER SHEAR DEFORMATION-THEORY FOR THE VIBRATION OF THICK PLATES [J].
HANNA, NF ;
LEISSA, AW .
JOURNAL OF SOUND AND VIBRATION, 1994, 170 (04) :545-555
[10]  
JONES RM, 1975, MECH COMPOSITE MAT, P31