Active control of thermal buckling and vibration for a sandwich composite laminated plate with piezoelectric fiber-reinforced composite actuator facesheets

The present paper is concerned with the active control of thermal buckling and vibration of a sandwich composite laminated plate with piezoelectric fiber-reinforced composite actuator facesheets in a thermal environment. An active temperature feedback control strategy is proposed for the thermal buckling of the composite sandwich plate. The results of numerical simulations show that the piezoelectric actuator can significantly improve the thermal buckling characteristics of the composite plates. The influence of the active thermal buckling control gain on the damping ratio and natural frequency of the structure is also investigated. From the numerical results it is observed that the active thermal buckling control with temperature feedback gain can not only enlarge the critical buckling temperature but can also reduce the resonant amplitude of the structure. Furthermore, the optimization problem is studied and it is found that the critical buckling temperature can be optimized by varying the fiber orientation in the piezoelectric fiber-reinforced composite layer. The active thermal buckling control method presented in this paper working in combination with the vibration control strategy can significantly improve the stability of the laminated composite plates. The present study will be useful for designing laminated composite structures used in the thermal environment.

[1]  Chuh Mei,et al.  THERMAL POSTBUCKLING OF COMPOSITE PLATES USING THE FINITE ELEMENT MODAL COORDINATE METHOD , 1999 .

[2]  M. Shariyat,et al.  Thermal buckling analysis of rectangular composite plates with temperature-dependent properties based on a layerwise theory , 2007 .

[3]  A. Waas,et al.  Thermal buckling of composite plates with spatial varying fiber orientations , 2015 .

[4]  M. Eslami,et al.  Thermal Buckling of Simply Supported Piezoelectric FGM Cylindrical Shells , 2007 .

[5]  Thermal buckling behavior of cross-ply hybrid composite laminates with inclined crack , 2006 .

[6]  Feng-Ming Li,et al.  Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow , 2017 .

[7]  P. Gonçalves,et al.  Active non-linear control of buckling and vibrations of a flexible buckled beam , 2002 .

[8]  Hui‐Shen Shen,et al.  Buckling and postbuckling of functionally graded graphene-reinforced composite laminated plates in thermal environments , 2017 .

[9]  Hui-Shen Shen,et al.  Postbuckling of FGM plates with piezoelectric actuators under thermo-electro-mechanical loadings , 2005 .

[10]  N. S. Viliani,et al.  Buckling Analysis of FG Plate with Smart Sensor/Actuator , 2009 .

[11]  Jie Yang,et al.  Postbuckling of piezoelectric FGM plates subject to thermo-electro-mechanical loading , 2003 .

[12]  H. Ovesy,et al.  Buckling and post-buckling analysis of delaminated piezo-composite material under electro-mechanical loading , 2016 .

[13]  Zhihua Wang,et al.  The effects of non-uniform temperature distribution and locally distributed anisotropic properties on thermal buckling of laminated panels , 2015 .

[14]  Hui‐Shen Shen,et al.  Postbuckling of pressure-loaded FGM hybrid cylindrical shells in thermal environments , 2007 .

[15]  Jinqiang Li,et al.  Analysis and optimal design for supersonic composite laminated plate , 2013 .

[16]  Yoshihiro Narita,et al.  Stochastic thermal buckling analysis of laminated plates using perturbation technique , 2016 .

[17]  M. Shariyat,et al.  Dynamic buckling of imperfect laminated plates with piezoelectric sensors and actuators subjected to thermo-electro-mechanical loadings, considering the temperature-dependency of the material properties , 2009 .

[18]  Hai Wang,et al.  Postbuckling of sandwich plates with graphene-reinforced composite face sheets in thermal environments , 2018 .

[19]  J. Loughlan,et al.  Buckling control using embedded shape memory actuators and the utilisation of smart technology in future aerospace platforms , 2002 .

[20]  L. Shiau,et al.  Thermal buckling behavior of composite laminated plates , 2010 .

[21]  Hiroyuki Matsunaga,et al.  Thermal buckling of angle-ply laminated composite and sandwich plates according to a global higher-order deformation theory , 2006 .

[22]  J. Loughlan,et al.  The control of the post-buckling response in thin composite plates using smart technology , 2000 .

[23]  J. Li,et al.  Vibration suppression for laminated composite plates with arbitrary boundary conditions , 2013, Mechanics of Composite Materials.

[24]  Sup Choi,et al.  Thermal buckling and postbuckling analysis of a laminated composite beam with embedded SMA actuators , 1999 .

[25]  Hui‐Shen Shen,et al.  Nonlinear free and forced vibration of simply supported shear deformable laminated plates with piezoelectric actuators , 2005 .

[26]  M. Ćetković Thermal buckling of laminated composite plates using layerwise displacement model , 2016 .

[27]  K. M. Liew,et al.  Transverse vibration of symmetrically laminated rectangular composite plates , 1992 .

[28]  J. Loughlan,et al.  The active buckling control of some composite column strips using piezoceramic actuators , 1995 .

[29]  Y. Narita Layerwise optimization for the maximum fundamental frequency of laminated composite plates , 2003 .

[30]  L. Dozio,et al.  Thermal Buckling Response of Laminated and Sandwich Plates using Refined 2-D Models , 2017 .

[31]  E. F. Joubaneh,et al.  Thermal buckling analysis of porous circular plate with piezoelectric actuators based on first order shear deformation theory , 2014 .

[32]  Robert M. Jones Thermal buckling of uniformly heated unidirectional and symmetric cross-ply laminated fiber-reinforced composite uniaxial in-plane restrained simply supported rectangular plates , 2005 .

[33]  Yoshihiro Narita,et al.  Vibration suppression for laminated cylindrical panels with arbitrary edge conditions , 2013 .