Vibration analysis of cross-ply laminated beams with general boundary conditions by Ritz method

被引:119
作者
Aydogdu, M [1 ]
机构
[1] Trakya Univ, MMF, Makine Muhendisligi Bolumu, TR-22030 Edirne, Turkey
关键词
cross-ply beams; vibration; Ritz method; general boundary conditions;
D O I
10.1016/j.ijmecsci.2005.06.010
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The present study is concerned with the vibration analysis of cross-ply laminated beams subjected to different sets of boundary conditions. The analysis is based on a three-degree-of-freedom shear deformable beam theory. The continuity conditions between layers of symmetric cross-ply laminated beams are satisfied by the use of the shape function incorporated into the theory which also unifies the ID shear deformable beam theories developed previously. The governing equations are obtained by means of Hamilton's principle. Six different combinations of free, clamped and simply supported edge boundary conditions are considered. The free vibration frequencies are obtained by applying the Ritz method where the three displacement components are expressed in a series of simple algebraic polynomials. The numerical results obtained for different length-to-thickness ratios and lay-ups are presented and compared with results available in the literature. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1740 / 1755
页数:16
相关论文
共 45 条
[1]   SHEAR DEFORMATION AND ROTARY INERTIA EFFECTS OF VIBRATING COMPOSITE BEAMS [J].
ABRAMOVICH, H .
COMPOSITE STRUCTURES, 1992, 20 (03) :165-173
[2]   FREE-VIBRATIONS OF NONSYMMETRICAL CROSS-PLY LAMINATED COMPOSITE BEAMS [J].
ABRAMOVICH, H ;
LIVSHITS, A .
JOURNAL OF SOUND AND VIBRATION, 1994, 176 (05) :597-612
[3]   A new zig-zag model for laminated composite beams: free vibration analysis [J].
Arya, H .
JOURNAL OF SOUND AND VIBRATION, 2003, 264 (02) :485-490
[4]   Vibration analysis of cross-ply laminated square plates with general boundary conditions [J].
Aydogdu, M ;
Timarci, T .
COMPOSITES SCIENCE AND TECHNOLOGY, 2003, 63 (07) :1061-1070
[5]   VIBRATION AND BUCKLING OF GENERALLY LAMINATED COMPOSITE PLATES WITH ARBITRARY EDGE CONDITIONS [J].
BAHARLOU, B ;
LEISSA, AW .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 1987, 29 (08) :545-555
[6]   Frequency equation and mode shape formulae for composite Timoshenko beams [J].
Banerjee, JR .
COMPOSITE STRUCTURES, 2001, 51 (04) :381-388
[7]   NATURAL FREQUENCIES OF RECTANGULAR-PLATES USING CHARACTERISTIC ORTHOGONAL POLYNOMIALS IN RAYLEIGH-RITZ METHOD [J].
BHAT, RB .
JOURNAL OF SOUND AND VIBRATION, 1985, 102 (04) :493-499
[8]   FREE-VIBRATION OF COMPOSITE BEAMS INCLUDING ROTARY INERTIA AND SHEAR DEFORMATION [J].
CHANDRASHEKHARA, K ;
KRISHNAMURTHY, K ;
ROY, S .
COMPOSITE STRUCTURES, 1990, 14 (04) :269-279
[9]   FREE-VIBRATION OF COMPOSITE BEAMS USING A REFINED SHEAR FLEXIBLE BEAM ELEMENT [J].
CHANDRASHEKHARA, K ;
BANGERA, KM .
COMPUTERS & STRUCTURES, 1992, 43 (04) :719-727
[10]   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