An assessment of Mixed and Classical Theories on Global and Local Response of Multilayered, Orthotropic Plates

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Variable kinematic models applied to free-vibration analysis of functionally graded material shells (2010, background): “K∗Û = ω(2) mnMÛ , (47) where K∗ is the equivalent stiffness matrix obtained by means of static condensation (for further details see [32], [33]), M is the inertial matrix and Û is the vector of unknown variables.”
On the free vibration analysis of laminated composite and sandwich plates: A review of recent literature with some numerical results (2015, background): “[19,20], Liu and Li [21], Carvelli and Savoia [22], Altenbach [23], Bose and Reddy [24,25], Carrera [26–29], Kant and Swaminathan [30], Chao and Chern [31], Ferreira and Fernandes [32], Kulikov [33], Ambartsumian [34], Piskunov and Rasskazov [35], Carrera and Demasi [36,37], Ghugal and Shimpi [38], ”
Mathematical modelling of a rectangular sandwich plate with a metal foam core (2011, background): “Carrera (2000, 2001, 2003) formulated the zig-zag hypotheses for multilayered plates.”
Thermal analysis of FGM plates – A critical review of various modeling techniques and solution methods (2017, background): “Carrera presented exhaustive comparative studies using more than 40 two dimensional theories in assessing the global and local response of multilayered plates and shells subjected to mechanical [4] and thermomechanical loads [5].”