journal article·2017-07

Geometrical nonlinear free vibration responses of FG-CNT reinforced composite annular sector plates integrated with piezoelectric layers

M. Mohammadzadeh-Keleshteri, H. Asadi, M.M. Aghdam

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Abstract

Abstract The objective of this research is to scrutinize large amplitude vibration response of functionally graded carbon nanotube reinforced composite (FG-CNTRC) annular sector plates with surface-bonded piezoelectric layers. A nonlinear formulation is derived based on the first-order shear deformation theory (FSDT), von Karman geometrical nonlinearity along with the Hamilton principle. The distribution of electric potential through the thickness of the piezoelectric layers is simulated by a sinusoidal function. The closed circuit electrical boundary condition is taken into consideration for the top and bottom surfaces of the piezoelectric layers. The nonlinear dynamic equations, boundary conditions and Maxwell equation are discretized using the generalized differential quadrature method and direct iterative method is then employed to solve the nonlinear system of equations. The variation of nonlinear frequency versus the vibration amplitude is highlighted considering various influential parameters such as distribution and volume fraction of the CNTs, geometrical parameters, boundary conditions and the thickness of the piezoelectric layers. It is found that the dynamic responses of the CNTRC sector plate may be noticeably enhanced by adjusting values of the CNT volume fraction and distribution. The numerical results reveal that the increase in the nonlinear frequency descents at certain vibration amplitude owing to vibration mode redistribution.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Nonlocal and gradient elasticity in micro/nano structures · Aeroelasticity and Vibration Control

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (74)

Show source-provided references
1. Analysis of wave propagation in piezoelectric coupled cylinder affected by transverse shear and rotary inertia10.1016/S0020-7683(03)00422-0 ↗
2. Free vibration analysis of piezoelectric coupled thin and thick annular plate10.1016/j.jsv.2004.01.009 ↗
3. Flexural vibration analysis of sandwich beam coupled with piezoelectric actuator10.1088/0964-1726/9/1/311 ↗
4. Analysis of piezoelectric coupled circular plate10.1088/0964-1726/10/2/308 ↗
5. Free vibration analysis of piezoelectric coupled circular plate with open circuit10.1016/j.jsv.2009.10.040 ↗
6. Analytical solution for free vibrations of moderately thick hybrid piezoelectric laminated plates10.1016/j.jsv.2013.05.010 ↗
7. Geometrically nonlinear transient thermos-elastic response of FG beams integrated with a pair of FG piezoelectric sensors10.1016/j.compstruct.2013.07.045 ↗
8. Large amplitude free vibration analysis of laminated composite spherical shells embedded with piezoelectric layers10.12989/sss.2015.16.5.853 ↗
9. Nonlinear transient analysis of smart laminated composite plate integrated with PVDF sensor and AFC actuator10.1016/j.compstruct.2016.08.020 ↗
10. Viswamurthy SR, Rao AK, Ganguli R. Dynamic hysteresis of piezoceramic stack actuators used in helicopter vibration control: experiments and simulation. Smart Mater Struct.
11. Active control of functionally graded laminated cylindrical shells10.1016/j.compstruct.2009.04.017 ↗
12. A FEM model for the active control of curved FGM shells using piezoelectric sensor-actuator layers10.1002/nme.451 ↗
13. Nonlinear free and forced vibration behavior of functionally graded plate with piezoelectric layers in thermal environment10.1016/j.compstruct.2011.03.019 ↗
14. Active control of FGM plates with integrated piezoelectric sensors and actuators10.1016/S0020-7683(00)00050-0 ↗
15. Active aeroelastic flutter analysis and vibration control of supersonic beams using piezoelectric actuator/sensor pairs10.1088/0964-1726/20/5/055013 ↗
16. Aerothermoelastic analysis and active flutter control of supersonic composite laminated cylindrical shells10.1016/j.compstruct.2013.07.029 ↗
17. Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate10.1016/j.compstruct.2011.09.005 ↗
18. Supersonic flutter suppression of piezolaminated cylindrical panels based on multifield layerwise theory10.1016/j.jsv.2005.07.033 ↗
19. Mechanical analysis of functionally graded carbon nanotube reinforced composites: a review10.1016/j.compstruct.2014.09.041 ↗
20. Deflection and stress behavior of nanocomposite reinforced beams using a multiscale analysis10.1016/j.compstruct.2005.09.011 ↗
21. Free vibrations and buckling analysis of carbon nanotube reinforced composite Timoshenko beams on elastic foundation10.1016/j.ijpvp.2012.07.012 ↗
22. Nonlinear analysis of nanotube reinforced composite beams resting on elastic foundations in thermal environments10.1016/j.engstruct.2013.06.002 ↗
23. Mehar K, Panda SK. Thermoelastic analysis of FG-CNT reinforced shear deformable composite plate under various loadings. Int J Comput Method, in press. http://dx.doi.org/10.1142/S0219876217500190.10.1142/S0219876217500190 ↗
24. Vibration of carbon nanotube reinforced composites beams based on the first and third order beam theories10.1016/j.apm.2014.02.008 ↗
25. Nonlinear forced vibration analysis of functionally graded carbon nanotube-reinforced composite Timoshenko beams10.1016/j.compstruct.2014.03.015 ↗
26. Nonlinear free vibration of functionally graded carbon nanotube-reinforced composite beams10.1016/j.compstruct.2009.09.024 ↗
27. Dynamic stability of functionally graded carbon nanotube reinforced composite beams10.1080/15376494.2011.581412 ↗
28. Numerical investigation of nonlinear thermomechanical deflection of functionally graded CNT reinforced doubly curved composite shell panel under different mechanical loads10.1016/j.compstruct.2016.10.135 ↗
29. Buckling analysis of functionally graded carbon nanotube-reinforced composite plates using the element-free kp-Ritz method10.1016/j.compstruct.2012.11.006 ↗
30. Large deflection analysis of functionally graded carbon nanotube-reinforced composite plates using the element-free kp-Ritz method10.1016/j.cma.2012.12.007 ↗
31. An element-free IMLS-Ritz framework for buckling analysis of FG-CNT reinforced composite thick plates resting on Winkler foundations10.1016/j.enganabound.2015.03.004 ↗
32. Buckling of FG-CNT reinforced composite thick skew plates resting on Pasternak foundations based on an element-free approach
33. Buckling analysis of FG-CNT reinforced composite thick skew plates using an element-free approach10.1016/j.compositesb.2015.01.033 ↗
34. Postbuckling analysis of carbon nanotube reinforced functionally graded cylindrical panels under axial compression using a meshless10.1016/j.cma.2013.09.001 ↗
35. Buckling and vibration analysis of a pressurized CNT reinforced functionally graded truncated conical shell under an axial compression using HDQ method10.1016/j.cma.2016.01.017 ↗
36. Large deflection geometrically nonlinear analysis of carbon nanotube reinforced functionally graded cylindrical panels10.1016/j.cma.2014.01.024 ↗
37. Static and dynamic of carbon nanotube reinforced functionally graded cylindrical panels10.1016/j.compstruct.2013.12.035 ↗
38. Computationally efficient model for flow-induced instability of CNT reinforced functionally graded truncated conical curved panels subjected to axial compression10.1016/j.cma.2017.02.020 ↗
39. Numerical study on the buckling and vibration of functionally graded carbon nanotube-reinforced composite conical shells under axial loading10.1016/j.compositesb.2016.03.080 ↗
40. On dynamic instability of a pressurized functionally graded carbon nanotube reinforced truncated conical shell subjected to yawed supersonic airflow10.1016/j.compstruct.2016.07.009 ↗
41. Thermal postbuckling of nanotube-reinforced composite cylindrical panels resting on elastic foundations in thermal environments10.1016/j.compstruct.2014.12.059 ↗
42. Nonlinear response of nanotube-reinforced composite cylindrical panels subjected to combined loadings and resting on elastic foundations10.1016/j.compstruct.2015.06.042 ↗
43. Thermal buckling and postbuckling behavior of functionally graded carbon nanotube-reinforced composite cylindrical shells10.1016/j.compositesb.2011.10.004 ↗
44. Three-dimensional free vibration analysis of functionally graded nanocomposite cylindrical panels reinforced by carbon nanotube10.1016/j.matdes.2013.01.001 ↗
45. Thermal buckling and postbuckling analysis of functionally graded carbon nanotube-reinforced composite beams10.4028/www.scientific.net/AMM.846.182 ↗
46. Asadi H, Wang Q. An investigation on the aeroelastic flutter characteristics of FG-CNTRC beams in the supersonic flow. Compos Part B; 2016 [in press]. http://dx.doi.org/10.1016/j.compositesb.2016.10.089.10.1016/j.compositesb.2016.10.089 ↗
47. Modeling of dynamic responses of CNT-reinforced composite cylindrical shells under impact loads10.1016/j.cma.2016.10.020 ↗
48. Free vibration of viscoelastic double-bonded polymeric nanocomposite plates reinforced by FG-SWCNTs using MSGT, sinusoidal shear deformation theory and meshless method10.1016/j.compstruct.2015.05.077 ↗
49. An element-free analysis of CNT-reinforced composite plates with column supports and elastically restrained edges under larger deformation10.1016/j.compositesb.2016.03.078 ↗
50. Vibration analysis of CNT-reinforced functionally graded composite cylindrical shell in thermal environments10.1016/j.ijmecsci.2016.06.020 ↗
51. Thermoelastic response of CNT reinforced cylindrical panel resting on elastic foundation using theory of elasticity10.1016/j.compositesb.2016.06.028 ↗
52. An efficient computational approach for size-dependent analysis of functionally graded nanoplates10.1016/j.cma.2015.07.021 ↗
53. Elasticity solution of free vibration and bending behavior of functionally graded carbon nanotube reinforced composite beam with thin piezoelectric layers using differential quadrature method10.1142/S1758825115400025 ↗
54. Free vibration analysis of functionally graded carbon nanotube reinforced composite cylindrical panel embedded in piezoelectric layers by using theory of elasticity10.1016/j.euromechsol.2013.10.002 ↗
55. Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow10.1016/j.cma.2015.11.029 ↗
56. Elasticity solution of functionally graded carbon nanotube-reinforced composite cylindrical panel subjected to thermo-mechanical load10.1016/j.compositesb.2015.09.060 ↗
57. Static analysis of functionally graded carbon nanotube reinforced composite plate embedded in piezoelectric layers by using theory of elasticity10.1016/j.compstruct.2012.08.018 ↗
58. Nonlinear dynamic stability of piezoelectric functionally graded carbon nanotube reinforced composite plates with initial geometric imperfection10.1016/j.ijnonlinmec.2013.10.011 ↗
59. Stability of carbon nanotube reinforced composite plates with surface bonded piezoelectric layers and under biaxial compression10.1016/j.compstruct.2014.01.040 ↗
60. Optimal shape control of CNT reinforced functionally graded composite plates using piezoelectric patches10.1016/j.compositesb.2015.09.044 ↗
61. Thermal bifurcation buckling of piezoelectric carbon nanotube reinforced composite beams10.1016/j.camwa.2013.04.031 ↗
62. A numerical study on flow-induced instabilities of supersonic FG-CNT reinforced composite flat panels in thermal environments10.1016/j.compstruct.2017.02.003 ↗
63. Enhanced thermal stability of functionally graded sandwich cylindrical shells by shape memory alloys10.1088/0964-1726/24/4/045022 ↗
64. Vibration analysis of axially moving line supported functionally graded plates with temperature-dependent properties10.1177/0954406213498033 ↗
65. Enhanced thermal buckling of laminated composite cylindrical shells with shape memory alloy10.1177/0021998315573287 ↗
66. Large amplitude vibration and post-buckling analysis of variable cross-section composite beams on nonlinear elastic foundation10.1016/j.ijmecsci.2013.11.017 ↗
67. Non-linear bending analysis of laminated sector plates using generalized differential quadrature10.1016/j.compstruct.2009.08.007 ↗
68. A generalized approach for implementing general boundary conditions in the GDQ free vibration of plates
69. Free vibration analysis of composite laminated conical shells by generalized differential quadrature10.1006/jsvi.1996.0379 ↗
70. Large amplitude free vibration of shear deformable laminated composite annular sector plates by a sector p-element10.1016/j.ijnonlinmec.2008.05.007 ↗
71. Levy type solution for free vibration analysis of functionally graded rectangular plates with piezoelectric layers10.1088/0964-1726/21/9/094017 ↗
72. Static and free vibration analyses of carbon nanotube-reinforced composite plates using finite element method with first order shear deformation plate theory10.1016/j.compstruct.2011.11.010 ↗
73. Geometrical nonlinear free vibration analysis of FG-CNT reinforced composite flat panel under uniform thermal field10.1016/j.compstruct.2016.02.038 ↗
74. Reddy · 2003