Benchmark 3D solution and assessment of a zigzag theory for free vibration of hybrid plates under initial electrothermomechanical stresses
Source abstract
Abstract
A benchmark three-dimensional (3D) exact piezothermoelasticity solution is presented for free vibration of simply supported cross-ply symmetrically laminated hybrid rectangular plates under initial in-plane electrothermomechanical stresses. The solution, based on second Piola stress tensor and nonlinear Lagrangian strains, accounts for the effect of initial transverse normal strain and the two-way electromechanical coupling. Benchmark results are presented for the natural frequencies under initial stresses and the modal distributions of displacements and stresses across the thickness, against which the accuracy of various 2D plate theories for hybrid plates can be assessed. A recently developed coupled 2D zigzag theory for hybrid plates is extended for the vibration under initial stresses. The theory uses a piecewise linear approximation for the thermal and potential fields across sublayers, and combines a global third-order variation with a piecewise linear (zigzag) variation across the layers for the inplane displacements. Using the conditions of continuity of transverse shear stresses at the layer interfaces and the shear traction-free conditions at the top and bottom, the number of primary displacement variables is reduced to five, as in the corresponding smeared third-order theory (TOT). The zigzag theory and the smeared TOT are assessed in comparison with the exact 3D solution for the natural frequencies and mode shapes of simply-supported rectangular plates under initial stresses. The zigzag theory results show excellent agreement with the 3D results when the initial thermal transverse normal strain is neglected, whereas the TOT may yield very inaccurate results depending upon the plate layup.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Railway Engineering and Dynamics · Acoustic Wave Phenomena Research
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References (37)
Show source-provided references
1. Three-dimensional solutions for the free vibrations and buckling of thermally stressed multilayered angle-ply composite plates10.1115/1.2894055 ↗
2. Three-dimensional solutions for initially stressed structural sandwiches10.1061/(ASCE)0733-9399(1994)120:2(284) ↗
3. Three-dimensional solutions for free vibrations of initially-stressed thermoelectroelastic multilayered plates10.1016/S0045-7825(96)01065-1 ↗
4. Exact 3D piezoelasticity solution for buckling of hybrid cross-ply plates using transfer matrices10.1007/s00707-004-0108-z ↗
5. Exact 3D piezothermoelasticity solution for buckling of hybrid cross-ply plates using state space approach10.1002/zamm.200310172 ↗
6. Buckling and dynamics of multilayered and laminated plates under initial stress10.1016/0020-7683(74)90111-5 ↗
7. Dynamic response of laminated composite plates under initial stress10.2514/3.7089 ↗
8. Free vibration of initially stressed composite laminates10.1016/0022-460X(90)90656-K ↗
9. Stability and vibration of initially stressed thick laminated plates10.1006/jsvi.1993.1374 ↗
10. Stability and vibration of initially stressed plates composed of spatially distributed fiber composites10.1006/jsvi.1996.0629 ↗
11. Vibration of cross-ply laminated composite plates subjected to initial in-plane stresses10.1016/S0263-8231(02)00012-5 ↗
12. Vibration of compressively loaded shear deformable flat panels exhibiting initial geometric imperfections10.2514/3.11305 ↗
13. Effects of geometric imperfections on vibration of compressed shear deformable laminated composite curved panels10.1007/BF01340710 ↗
14. Frequency-load interaction of geometrically imperfect curved panels subjected to heating10.2514/3.13037 ↗
15. Dynamic response of initially stressed functionally graded rectangular thin plates10.1016/S0263-8223(01)00122-2 ↗
16. Stiffening effects on the free vibration behavior of composite plates with PZT actuators10.1016/S0263-8223(99)00125-7 ↗
17. Stiffening effects on the natural frequencies of laminated plates with piezoelectric actuators10.1016/S1359-8368(02)00026-4 ↗
18. Damped vibration of composite plates with passive piezoelectric-resistor elements10.1006/jsvi.1998.2037 ↗
19. A refined hybrid plate theory for composite laminates with piezoelectric laminae10.1016/0020-7683(94)00229-P ↗
20. Coupled discrete-layer finite elements for laminated piezoelectric plates10.1002/cnm.1640101203 ↗
21. Layerwise mechanics and finite element for the dynamic analysis of piezoelectric composite plates10.1016/S0020-7683(96)00012-1 ↗
22. Coupled high-order shear layerwise analysis of adaptive sandwich piezoelectric composite Beams10.2514/1.12269 ↗
23. An improved Reissner–Mindlin type model for the electromechanical analysis of multilayered plates including piezo-layers10.1177/1045389X9700800305 ↗
24. A coupled zigzag third-order theory for hybrid cross-ply plates10.1115/1.1767170 ↗
25. Nonlinear zigzag theory for electrothermomechanical buckling of piezoelectric composite and sandwich plates10.1007/s00707-006-0318-7 ↗
26. Higher-order zig-zag theory for fully coupled thermo-electro-mechanical smart composite plates10.1016/j.ijsolstr.2003.10.020 ↗
27. Mechanics and computational models for laminated piezoelectric beams, plates and shells10.1115/1.3098918 ↗
28. Higher-order zigzag model for analysis of thick composite beams with inclusion of transverse normal stress and sublaminates approximations10.1016/S1359-8368(01)00016-6 ↗
29. Applications of zigzag theories to sandwich beams10.1080/15376490306737 ↗
30. C0 plate element for global/local analysis of multilayered composites, based on a 3D zigzag model and strain energy updating10.1016/j.ijmecsci.2005.06.002 ↗
31. Mal · 1990
32. Auld · 1973 · vol. I
33. Achary GGS. Coupled exact 3D solutions and 2D zigzag theory for thermo-electro-mechanical analysis of hybrid piezoelectric plates. PhD Thesis, Indian Institute of Technology, Delhi, India, 2005.
34. Exact free-vibration analysis of laminated plates with embedded piezoelectric layers10.1121/1.413420 ↗
35. Petyt · 1990
36. Thick beam theory and finite element model with zig-zag sublaminate approximations10.2514/3.13281 ↗
37. Three-dimensional solutions for coupled thermoelectroelastic response of multilayered plates10.1016/0045-7825(95)00825-L ↗