A comparison of buckling and postbuckling behavior of FGM plates with piezoelectric fiber reinforced composite actuators
Source abstract
Abstract
Abstract Compressive postbuckling under thermal environments and thermal postbuckling due to a uniform temperature rise are presented for a simply supported, shear deformable functionally graded plate with piezoelectric fiber reinforced composite (PFRC) actuators. The material properties of functionally graded materials (FGMs) are assumed to be graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents, and the material properties of both FGM and PFRC layers are assumed to be temperature-dependent. The governing equations are based on a higher order shear deformation plate theory that includes thermo-piezoelectric effects. The initial geometric imperfection of the plate is taken into account. A two step perturbation technique is employed to determine buckling loads (temperature) and postbuckling equilibrium paths. The numerical illustrations concern the compressive and thermal postbuckling behaviors of perfect and imperfect, geometrically mid-plane symmetric FGM plates with fully covered or embedded PFRC actuators under different sets of thermal and electric loading conditions. The results for monolithic piezoelectric actuator, which is a special case in the present study, are compared with those of PFRC actuators. The results reveal that, in the compressive buckling case, the applied voltage usually has a small effect on the postbuckling load–deflection curves of the plate with PFRC actuators, whereas in the thermal buckling case, the effect of applied voltage is more pronounced for the plate with PFRC actuators, compared to the results of the same plate with monolithic piezoelectric actuators.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Aeroelasticity and Vibration Control · Structural Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (36)
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1. Active control of FGM plates with integrated piezoelectric sensors and actuators10.1016/S0020-7683(00)00050-0 ↗
2. Active control of FGM plates subjected to a temperature gradient: modelling via finite element method based on FSDT10.1002/nme.252 ↗
3. Finite element piezothermoelasticity analysis and the active control of FGM plates with integrated piezoelectric sensors and actuators10.1007/s00466-003-0437-0 ↗
4. Nonlinear analysis of functionally graded plates under transverse and in-plane loads10.1016/S0020-7462(01)00070-1 ↗
5. Imperfection sensitivity of the post-buckling behavior of higher-order shear deformable functionally graded plates10.1016/j.ijsolstr.2005.06.061 ↗
6. Thermomechanical postbuckling analysis of moderately thick functionally graded plates and shallow shells10.1016/j.ijmecsci.2005.04.008 ↗
7. Post-buckling analysis of functionally graded rectangular plates10.1016/j.compstruct.2005.08.026 ↗
8. Thermal postbuckling and vibration analyses of functionally graded plates10.1016/j.jsv.2005.01.031 ↗
9. Thermal postbuckling analysis of FGM skew plates10.1016/j.engstruct.2007.02.012 ↗
10. Postbuckling response of functionally graded rectangular plates subjected to thermo-mechanical loading10.1142/S0219455407002381 ↗
11. Nonlinear bending response of functionally graded plates subjected to transverse loads and in thermal environments10.1016/S0020-7403(01)00103-5 ↗
12. Conditions for laminated plates to remain flat under inplane loading10.1016/0263-8223(86)90022-X ↗
13. Buckling or transverse deflections of unsymmetrically laminated plates subjected to in-plane loads10.2514/3.11336 ↗
14. Conditions for functionally graded plates to remain flat under in-plane loads by classical plate theory10.1016/j.compstruct.2006.10.004 ↗
15. Postbuckling of piezoelectric FGM plates subject to thermo-electro-mechanical loading10.1016/S0020-7683(03)00096-9 ↗
16. Stability of functionally graded hybrid composite plates10.1016/0961-9526(95)00036-M ↗
17. Buckling analysis of functionally graded plates subjected to uniaxial loading10.1016/S0263-8223(97)00038-X ↗
18. Postbuckling of FGM plates with piezoelectric actuators under thermo-electro-mechanical loadings10.1016/j.ijsolstr.2005.03.042 ↗
19. Stability of piezoelectric FGM rectangular plates subjected to non-uniformly distributed load, heat and voltage10.1016/j.advengsoft.2006.12.004 ↗
20. Effective coefficients of piezoelectric fiber-reinforced composites10.2514/2.2001 ↗
21. Finite element analysis of smart functionally graded plates10.1016/j.ijsolstr.2005.06.096 ↗
22. Nonlinear analysis of smart functionally graded plates integrated with a layer of piezoelectric fiber reinforced composite10.1088/0964-1726/15/6/011 ↗
23. Nonlinear vibration and dynamic response of FGM plates with piezoelectric fiber reinforced composite actuators10.1016/j.compstruct.2009.03.018 ↗
24. Thermal postbuckling behavior of shear deformable FGM plates with temperature-dependent properties10.1016/j.ijmecsci.2006.09.011 ↗
25. Tsai · 1980
26. Reddy · 2004
27. Thermomechanical analysis of functionally graded cylinders and plates10.1080/01495739808956165 ↗
28. Exact free vibration analysis of laminated plates with embedded piezoelectric layers10.1121/1.413420 ↗
29. Large-deflection and strain analysis of multilayered plates with induced-strain actuators10.1088/0964-1726/5/2/004 ↗
30. An improved Reissner–Mindlin-type model for the electromechanical analysis of multilayered plates including piezo-layers10.1177/1045389X9700800305 ↗
31. On laminated composite plates with integrated sensors and actuators10.1016/S0141-0296(97)00212-5 ↗
32. A simple higher-order theory for laminated composite plates10.1115/1.3167719 ↗
33. Shen · 2009
34. Three-dimensional vibrations of laminated piezoelectric cylinders10.1061/(ASCE)0733-9399(1998)124:11(1294) ↗
35. Touloukian · 1967
36. Thermal buckling of functionally graded plates based on higher order theory10.1080/01495730290074333 ↗