Influence of openings and additional mass on vibration of laminated sandwich rhombic plates using IHSDT

被引:12
作者
Anish [1 ]
Kumar, Ajay [1 ]
Chakrabarti, Anupam [2 ]
机构
[1] Natl Inst Technol, Dept Civil Engn, Patna 800005, Bihar, India
[2] Indian Inst Technol Roorkee, Dept Civil Engn, Roorkee, Uttarakhand, India
关键词
Sandwich plate; finite element method; improved higher order shear deformation theory; skew angle; mode shape; HIGHER-ORDER THEORY; COMPOSITE PLATES; RECTANGULAR-PLATES; DYNAMIC-RESPONSE; CUT-OUTS; DEFORMATION; STABILITY; FORMULATION;
D O I
10.1177/0892705718785682
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this article, investigations on the influence of openings and additional mass on free vibration analysis of laminated composite sandwich skew plates using improved higher order shear deformation theory (IHSDT) have been done. The IHSDT model satisfies the interlaminar shear stress continuity at the layer interfaces and also ensures zero transverse shear stress conditions at the top and bottom of the plate. The piecewise parabolic shear stress variation across the thickness of each layer is considered. No shear correction factors are required. The 2-D C-0 finite element (FE) model has been developed by authors based on IHSDT. FE model based on IHSDT has been coded in FORTRAN. The problem of C-1 continuity requirement associated with the IHSDT is overcome using an appropriate C-0 FE formulation. The free vibration frequencies of laminated composite and sandwich plates obtained using the present 2-D FE model are in good agreement with the 3-D elasticity results. The influence of the side-to-thickness ratio, skew angles, boundary conditions, and mode shapes is taken into consideration for the present study.
引用
收藏
页码:3 / 34
页数:32
相关论文
共 47 条
[1]   PREDICTION OF NATURAL FREQUENCIES OF VIBRATION OF RECTANGULAR-PLATES WITH RECTANGULAR CUTOUTS [J].
ALI, R ;
ATWAL, SJ .
COMPUTERS & STRUCTURES, 1980, 12 (06) :819-823
[2]   Free vibration of composite plates with mixed boundary conditions based on higher-order shear deformation theory [J].
Asadi, E. ;
Fariborz, S. J. .
ARCHIVE OF APPLIED MECHANICS, 2012, 82 (06) :755-766
[3]  
Ashton JE, 1970, THEORY LAMINATED PLA, P153
[4]  
Bathe KJ, FINITE ELEMENT METHO
[5]  
CHAI GB, 1996, COMPOS STRUCT, V35, P357
[6]   Vibration of laminate-faced sandwich plate by a new refined element [J].
Chakrabarti, A ;
Sheikh, AH .
JOURNAL OF AEROSPACE ENGINEERING, 2004, 17 (03) :123-134
[7]   Vibration analysis of symmetrically laminated thick rectangular plates using the higher-order theory and p-Ritz method [J].
Chen, CC ;
Liew, KM ;
Lim, CW ;
Kitipornchai, S .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1997, 102 (03) :1600-1611
[8]   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
[9]   Buckling and vibration analysis of isotropic and laminated plates by radial basis functions [J].
Ferreira, A. J. M. ;
Roque, C. M. C. ;
Neves, A. M. A. ;
Jorge, R. M. N. ;
Soares, C. M. M. ;
Liew, K. M. .
COMPOSITES PART B-ENGINEERING, 2011, 42 (03) :592-606
[10]   Analysis of thick isotropic and cross-ply laminated plates by radial basis functions and a Unified Formulation [J].
Ferreira, A. J. M. ;
Roque, C. M. C. ;
Carrera, E. ;
Cinefra, M. .
JOURNAL OF SOUND AND VIBRATION, 2011, 330 (04) :771-787