Theories and finite elements for multilayered, anisotropic, composite plates and shells

By Erasmo Carrera. 2002

915 citations recorded by the source corpus.

Subfields: Civil and Structural Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/6255b7ea7aeeea2a983541e5a9ae1160bc75cebf

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In Civil and Structural Engineering

In Mechanics of Materials

Citations in the corpus

Advanced mixed theories for bending analysis of functionally graded plates (2010, background): “1 and 2 are formally the same that have been obtained for ‘‘classical” multilayer plate [17,18], the only difference is the index r that represents the assembling procedure for FGM layers.”
Theories and Finite Elements for Multilayered Plates and Shells:A Unified compact formulation with numerical assessment and benchmarking (2003, background): “(i) – To give some inside for a certain class of two–dimensional models mentioned in [ 1 ] by discussing in unified manner the derivation and implementation of differential governing equations and finite element matrices; (ii) – To quote a detailed numerical evaluation of available results along wit”
An equivalent layer-wise approach for the free vibration analysis of thick and thin laminated and sandwich shells (2016, background): “In the review paper [57] a complete treatise about both ESL and LW approaches is presented.”
A Bending-Gradient model for thick plates. Part I: Theory (2011, background): “The reader can refer to Reddy (1989) and Carrera (2002) for detailed reviews.”
Radial basis functions-finite differences collocation and a Unified Formulation for bending, vibration and buckling analysis of laminated plates, according to Murakami's zig-zag theory (2011, background): “…Porto, Portugal c Department of Aeronautics and Aerospace Engineering, Politecnico di Torino, Corso Duca degli Abruzzi, 24, 10129 Torino, Italy a r t i c l e i n f o a b s t r a c t Article history: Available online 20 January 2011 Keywords: Radial basis functions Finite differences Zig-zag theory…”
Performance of CUF Approach to Analyze the Structural Behavior of Slender Bodies (2012, neutral): “This formulation has been developed over the last decade for plate/ shell models (Carrera 1995, 2002, 2003; Carrera et al. 2008), and it has recently been extended to beam modelings (Carrera and Giunta 2010).”
A unified formulation for finite element analysis of piezoelectric adaptive plates (2006, background): “This formulation has already shown all its potentiality as a base for finite elements in the mechanical [10,11] and thermoelastic analysis [12] of multilayered plates.”
Accurate free vibration analysis of thermo-mechanically pre/post-buckled anisotropic multilayered plates based on a refined hierarchical trigonometric Ritz formulation (2013, background): “During the last two decades a wide range of classical and mixed 2D plate/shell theories has been developed by Carrera [34–39], who proposed the Carrera unified formulation (CUF) with the purpose to overcome the limits which are typical of the equivalent single layer (ESL) models.”
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], ”
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev polynomials (2015, neutral): “The CUF has been developed for plates and shell analysis [31, 32].”
Refined One-Dimensional Formulations for Laminated Structure Analysis (2012, background): “CUFwas initially proposed for higher-order plate and shell models [57,58].”