Frequency and mode change in the large deflection and post-buckling of compact and thin-walled beams

Abstract This paper deals with the investigation of normal modes change of metallic structures, when subjected to geometrical nonlinearities in the large displacement/rotations field. Namely, a unified framework based on the Carrera Unified Formulation (CUF) and a total Lagrangian approach are employed to formulate higher order beam theories including geometric nonlinearities. Thus, a finite element approximation is used along with a path-following method to perform nonlinear analyses. Linearized vibration modes around equilibrium states and along the whole equilibrium path of structures subjected to bending and compression loadings are evaluated by solving a classical eigenvalue problem. In order to show the capabilities of the proposed methodology, both solid and thin-walled cross-section beams are considered. The analyses demonstrate that, with some differences depending on the geometry and both boundary and loading conditions, natural frequencies and modal shapes may change significantly as the structure is subjected to large displacements and rotations.

[1]  Pizhong Qiao,et al.  On an exact bending curvature model for nonlinear free vibration analysis shear deformable anisotropic laminated beams , 2014 .

[2]  Erasmo Carrera,et al.  Advanced beam formulations for free-vibration analysis of conventional and joined wings , 2012 .

[3]  Erasmo Carrera,et al.  Component-wise analysis of laminated anisotropic composites , 2012 .

[4]  Erasmo Carrera,et al.  Free vibration analysis of civil engineering structures by component-wise models , 2014 .

[5]  K. Liew,et al.  Nonlinear free vibration, postbuckling and nonlinear static deflection of piezoelectric fiber-reinforced laminated composite beams , 2014 .

[6]  Erasmo Carrera,et al.  Finite Element Analysis of Structures through Unified Formulation , 2014 .

[7]  N. Yamaki,et al.  Non-linear vibrations of a clamped beam with initial deflection and initial axial displacement, Part II: Experiment , 1980 .

[8]  Erasmo Carrera,et al.  Dynamic response of aerospace structures by means of refined beam theories , 2015 .

[9]  R. Ogden,et al.  The effect of pre-stress on the vibration and stability of elastic plates , 1993 .

[10]  Gangan Prathap,et al.  Galerkin finite element method for non-linear beam vibrations , 1980 .

[11]  Ali H. Nayfeh,et al.  Experimental Validation of Reduction Methods for Nonlinear Vibrations of Distributed-Parameter Systems: Analysis of a Buckled Beam , 1998 .

[12]  John Dugundji,et al.  Nonlinear Vibrations of a Buckled Beam Under Harmonic Excitation , 1971 .

[13]  Da Chen,et al.  Nonlinear free vibration of shear deformable sandwich beam with a functionally graded porous core , 2016 .

[14]  Li-Qun Chen,et al.  Galerkin methods for natural frequencies of high-speed axially moving beams , 2010 .

[15]  H. Abramovich,et al.  Buckling prediction of panels using the vibration correlation technique , 2015 .

[16]  Erasmo Carrera,et al.  Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation , 2017 .

[17]  Ranjan Ganguli,et al.  Nonlinear vibration analysis of composite laminated and sandwich plates with random material properties , 2010 .

[18]  S. Timoshenko Theory of Elastic Stability , 1936 .

[19]  Erasmo Carrera,et al.  Unified formulation of geometrically nonlinear refined beam theories , 2018 .

[20]  M. Chandrashekhar,et al.  Damage assessment of structures with uncertainty by using mode-shape curvatures and fuzzy logic , 2009 .

[21]  Ahmad Reza Ghasemi,et al.  Nonlinear free vibration of an Euler-Bernoulli composite beam undergoing finite strain subjected to different boundary conditions , 2016 .

[22]  A. Leissa,et al.  Vibration of shells , 1973 .

[23]  N. Yamaki,et al.  Non-linear vibrations of a clamped beam with initial deflection and initial axial displacement, Part I: Theory , 1980 .

[24]  Erasmo Carrera,et al.  Refined beam elements with only displacement variables and plate/shell capabilities , 2012 .

[25]  Maurice A. Biot,et al.  XLIII. Non-linear Theory of Elasticity and the linearized case for a body under initial stress , 1939 .

[26]  E. Carrera,et al.  Dynamic Analyses of Axisymmetric Rotors Through Three-Dimensional Approaches and High-Fidelity Beam Theories , 2017 .

[27]  Seng Tjhen Lie,et al.  Detection of damaged supports under railway track based on frequency shift , 2017 .

[28]  M. M. Aghdam,et al.  Nonlinear free vibration and post-buckling analysis of functionally graded beams on nonlinear elastic foundation , 2011 .

[29]  Erasmo Carrera,et al.  Application of a Refined Multi-Field Beam Model for the Analysis of Complex Configurations , 2015 .

[30]  Gaetano Giunta,et al.  Beam Structures: Classical and Advanced Theories , 2011 .

[31]  Lawrence N. Virgin,et al.  Vibration of Axially-Loaded Structures , 2007 .

[32]  Harold Lurie,et al.  Lateral vibrations as related to structural stability , 1950 .

[33]  J. R. Banerjee,et al.  Exact dynamic stiffness elements based on one-dimensional higher-order theories for free vibration analysis of solid and thin-walled structures , 2013 .

[34]  A. Leissa,et al.  Vibrations of continuous systems , 2011 .

[35]  K. E. Bisshopp,et al.  Large deflection of cantilever beams , 1945 .

[36]  Mohammad Mohammadi Aghdam,et al.  Large amplitude vibration and post-buckling analysis of variable cross-section composite beams on nonlinear elastic foundation , 2014 .

[37]  K. Bathe Finite Element Procedures , 1995 .