Large amplitude vibration analysis of composite beams: Simple closed-form solutions

被引:54
作者
Gunda, Jagadish Babu [1 ]
Gupta, R. K. [1 ]
Janardhan, G. Ranga [2 ]
Rao, G. Venkateswara [3 ]
机构
[1] Adv Syst Lab, Hyderabad 500058, Andhra Pradesh, India
[2] JNTU Coll Engn, Kakinada 533003, India
[3] Sreenidhi Inst Sci & Technol, Hyderabad 501301, Andhra Pradesh, India
关键词
Nonlinear vibration; Quadratic and cubic nonlinearity; Rayleigh-Ritz method; Coupled displacement field; Composite beam; FUNCTIONALLY GRADED BEAMS; NONLINEAR VIBRATIONS; FORCED VIBRATIONS; ELEMENT; PLATES;
D O I
10.1016/j.compstruct.2010.07.006
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Large amplitude vibration analysis of laminated composite beam with axially immovable ends is investigated with symmetric and asymmetric layup orientations by using the Rayleigh-Ritz (R-R) method The displacement fields used in the analytical formulation are coupled by using the homogeneous governing static axial equilibrium equation of the beam Geometric nonlinearity of von-Karman type is considered which accounts for the membrane stretching action of the beam The simple closed-form solutions are presented for the nonlinear harmonic radian frequency as function of central amplitude of the beam using the R-R method The nonlinear harmonic radian frequency results obtained from the closed-form solutions of the R-R method in general show good agreement with the results obtained from simple iterative finite element formulation Furthermore, the closed-form expressions are corrected for the harmonic motion assumption from the available literature results on the existence of quadratic and cubic nonlinearity It is interesting to note that the composite beams can result in asymmetric frequency vs amplitude curves depending upon the nature of direction of displacement in contrast to isotropic beams which exhibit cubic nonlinearity only and leads to symmetric frequency vs amplitude curves with respect to sign of the amplitude (C) 2010 Elsevier Ltd All rights reserved
引用
收藏
页码:870 / 879
页数:10
相关论文
共 34 条
[1]  
[Anonymous], 2004, INTRO NONLINEAR FINI, DOI DOI 10.1093/ACPROF:OSO/978019-8525295.003.0002
[2]   Free and forced vibrations of non-uniform composite beams [J].
Calim, Faruk Firat .
COMPOSITE STRUCTURES, 2009, 88 (03) :413-423
[3]   Nonlinear vibration of laminated plates on a nonlinear elastic foundation [J].
Chien, RD ;
Chen, CS .
COMPOSITE STRUCTURES, 2005, 70 (01) :90-99
[4]   A static and dynamic analysis of the postbuckling of geometrically imperfect composite beams [J].
Emam, Samir A. .
COMPOSITE STRUCTURES, 2009, 90 (02) :247-253
[5]   Postbuckling and free vibrations of composite beams [J].
Emam, Samir A. ;
Nayfeh, Ali H. .
COMPOSITE STRUCTURES, 2009, 88 (04) :636-642
[6]   Free vibration analysis of simply supported composite laminated panels [J].
Ganapathi, M. ;
Kalyani, Amit ;
Mondal, Bhaskar ;
Prakash, T. .
COMPOSITE STRUCTURES, 2009, 90 (01) :100-103
[7]   Application of spline element for large-amplitude free vibrations of laminated orthotropic straight/curved beams [J].
Ganapathi, M ;
Patel, BP ;
Saravanan, J ;
Touratier, M .
COMPOSITES PART B-ENGINEERING, 1998, 29 (01) :1-8
[8]   Post-buckling analysis of composite beams: Simple and accurate closed-form expressions [J].
Gupta, R. K. ;
Gunda, Jagadish Babu ;
Janardhan, G. Ranga ;
Rao, G. Venkateswara .
COMPOSITE STRUCTURES, 2010, 92 (08) :1947-1956
[9]   Thermal post-buckling analysis of slender columns using the concept of coupled displacement field [J].
Gupta, R. K. ;
Gunda, Jagadish Babu ;
Janardhan, G. Ranga ;
Rao, G. Venkateswara .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2010, 52 (04) :590-594
[10]   Relatively simple finite element formulation for the large amplitude free vibrations of uniform beams [J].
Gupta, R. K. ;
Babu, Gunda Jagadish ;
Janardhan, G. Ranga ;
Rao, G. Venkateswara .
FINITE ELEMENTS IN ANALYSIS AND DESIGN, 2009, 45 (10) :624-631