2019
DOI: 10.1016/j.euromechsol.2018.11.013
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Buckling and free vibration analysis of piezoelectric laminated composite plates using various plate deformation theories

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Cited by 29 publications
(7 citation statements)
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“…Q ̂ 11 and Q ̂ 22 are the reduced elastic stiffness coefficients, e ̂ 31 and η 33 are the reduced piezoelectric and dielectric coefficients, respectively. The reduced piezoelectric and dielectric coefficients can be obtained from Tanzadeh and Amoushahi (2019). The displacement field of the beam is represented by first order shear deformation theory (FSDT).…”
Section: Mathematical Formulationmentioning
confidence: 99%
“…Q ̂ 11 and Q ̂ 22 are the reduced elastic stiffness coefficients, e ̂ 31 and η 33 are the reduced piezoelectric and dielectric coefficients, respectively. The reduced piezoelectric and dielectric coefficients can be obtained from Tanzadeh and Amoushahi (2019). The displacement field of the beam is represented by first order shear deformation theory (FSDT).…”
Section: Mathematical Formulationmentioning
confidence: 99%
“…In addition, some analytical and semi-analytical methods are used for the dynamic analysis of piezoelectric laminated plates. Tanzadeh and Amoushahi [ 19 ] developed a finite strip method to analyze the free vibration of piezoelectric laminated plates based on Zigzag theory, refined plate and higher order shear deformation theory. Andakhshideh et al [ 20 ] studied the interlaminar stresses of laminated piezoelectric plates.…”
Section: Introductionmentioning
confidence: 99%
“…Ellali et al [7] found Navier's solution for the buckling response of the electro-magneto-elastic plates resting on an elastic foundation based on the third-order shear deformation theory (TSDT). On the order hand, according to the various plate theory, Tanzadeh et al [8] presented the buckling and vibration of the piezoelectric laminated composite plate based on the finite strip method. Based on the finite element method and Euler-Bernoulli beam theory, El Harti et al [9] used the analytical method to study the active vibration control of the FG beams with piezoelectric sensors and actuators.…”
Section: Introductionmentioning
confidence: 99%