2019
DOI: 10.1080/15376494.2018.1553259
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Geometrically nonlinear free vibration analysis of laminated composite plates: A finite element assessment of a higher order non-polynomial shear deformation theory

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Cited by 15 publications
(9 citation statements)
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“…Next, the validation of the nonlinear frequency ratio of an eight layer simply supported cross-ply laminate true[true( 0/ 90true)2true]s is presented in Table 2 together with the results of Ganapathi et al. 45 and Adhikari and Dash 16 and both the solutions are well matching with each other. The frequency ratio of the laminate is increasing with an increase in the amplitude of vibration i.e.…”
Section: Resultsmentioning
confidence: 87%
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“…Next, the validation of the nonlinear frequency ratio of an eight layer simply supported cross-ply laminate true[true( 0/ 90true)2true]s is presented in Table 2 together with the results of Ganapathi et al. 45 and Adhikari and Dash 16 and both the solutions are well matching with each other. The frequency ratio of the laminate is increasing with an increase in the amplitude of vibration i.e.…”
Section: Resultsmentioning
confidence: 87%
“…By applying equations (6) to (8), equation (11) can be rewritten as Now, by substituting the equations (5) and (7) and following the procedure explained in Adhikari and Dash, 16 equation (12) can further be modified as…”
Section: Mathematical Formulationmentioning
confidence: 99%
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