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This paper reports an investigation of the influence of initial stress on the flexural vibration of an individual multi-wall carbon nanotube with simply supported ends, based on a laminated elastic beam model considering the van der Waals force interaction between two adjacent nanotubes.
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This paper deals with the local global analysis of laminated composite and sandwich plates using a layerwise displacement model [Reddy JN. A plate bending element based on a generalized laminated plate theory. Int J Numer Methods Eng 1989 28 2275 92].
Buckling, material failure and ultimate collapse of the stiffened panels are predicted by nonlinear finite element analysis, which is based on a degenerated three-dimensional laminated composite shell element with updated Lagrangian formulation and first-order shear deformable kinematics.
To support the engineering of laminated composite structures, this work developed a novel Semantic LAminated Composites Knowledge management System (SLACKS) that is based on a suite of ontologies for laminated composites materials and design for manufacturing (DFM) and their integration into a previously developed engineering design framework.
Vibration and stability results for a laminated plate based on a modified higher order plate theory with seven kinematic variables are presented.
In the present contribution, particular attention is devoted to the fabrication and characterization of fully bio laminated structures based on a commercial poly (lactic acid) (PLA) including a jute fabric as reinforcements, even because of the limited availability of the reference literature.
A two-dimensional finite element model is presented to perform the linear static analysis of laminated orthotropic composite plates based on a refined higher order shear deformation theory.
In the framework of von Kármán type of kinematic nonlinearity, the motion equations of an FG-GRC laminated plate are established based on a higher-order shear deformation theory and solved by a two-step perturbation technique.
Based on a modified couple stress theory, a model for composite laminated beam with first order shear deformation is developed.
In this work, we extend a previously developed four-node quadrilateral element for laminated plates based on an efficient layerwise theory, called the zigzag theory (ZIGT), to laminated shallow shells.
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