2015
DOI: 10.1016/j.commatsci.2014.04.068
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Analysis of laminated composite plates integrated with piezoelectric sensors and actuators using higher-order shear deformation theory and isogeometric finite elements

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Cited by 140 publications
(49 citation statements)
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“…The piezoelectric layers have a thickness of 0.1 mm and are made of PZTG1195N (material properties in Table 3). Figure 5 displays the central line deflection of the considered structure subjected to the combined excitation involving the uniform load and different input voltages of 0, 5 and 10 V. The obtained results agree well with those obtained by (Phung- Van et al, 2015) and (Liu et al, 2004) (Table 1).…”
Section: Simple Supported Piezoelectric Composite Plate (Sym)supporting
confidence: 82%
“…The piezoelectric layers have a thickness of 0.1 mm and are made of PZTG1195N (material properties in Table 3). Figure 5 displays the central line deflection of the considered structure subjected to the combined excitation involving the uniform load and different input voltages of 0, 5 and 10 V. The obtained results agree well with those obtained by (Phung- Van et al, 2015) and (Liu et al, 2004) (Table 1).…”
Section: Simple Supported Piezoelectric Composite Plate (Sym)supporting
confidence: 82%
“…tic properties of Graphite/Epoxy are [19] [20] . The effect of the grid point number in DQM on the dimensionless nonlinear frequency (i.e., Ω = ω ρh 2 /E 11 ) of the laminated plate is demonstrated in Fig.…”
Section: Dqmmentioning
confidence: 99%
“…Willberg and Gabbert (2012) proposed solid NURBS-based IGA piezoelectric elements. While Phung- Van et al (2015), developed IGA shell for laminated composite plates with piezoelectric layers employing Higher-order Shear Deformation Theory (HSDT). Those models however limited to the application of sensors and actuators.…”
Section: Introductionmentioning
confidence: 99%