Agglomeration effects on the dynamic buckling of viscoelastic microplates reinforced with SWCNTs using Bolotin method

Kolahchi, Reza; Cheraghbak, Ali

doi:10.1007/s11071-017-3676-x

Cited by 28 publications

(8 citation statements)

References 31 publications

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“…By placing the solutions (32)(33)(34) into the equations (40,41) and then putting the resulting expressions into equation 31, the average end-shortening displacements are obtained as…”

Section: Formulationsmentioning

confidence: 99%

“…Kiani and coworker 36,37 made use of a nonuniform rational B-spline-based isogeometric finite element method to study the thermal buckling and postbuckling responses of graphene-reinforced laminated plates. Basing on numerical methods, dynamic stability of nanocomposite plates has been addressed in works of Kolahchi and collaborators 38 –43 including the effects of viscidity, piezoelectric layers, CNT agglomeration, orthotropic elastomeric medium, and temperature-dependent properties. Making use of asymptotic solutions and a perturbation technique, Shen and Xiang 44 and Shen 45 investigated thermal postbuckling behaviors of FG-CNTRC cylindrical panels and circular cylindrical shells subjected to uniform temperature rise, respectively.…”

Section: Introductionmentioning

confidence: 99%

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Thermal postbuckling of shear deformable CNT-reinforced composite plates with tangentially restrained edges and temperature-dependent properties

Tung

Trang

2018

Journal of Thermoplastic Composite Materials

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Buckling and postbuckling behaviors of moderately thick composite plates reinforced by single-walled carbon nanotubes (SWCNTs), rested on elastic foundations and subjected to two types of thermal loading are investigated in this article. Carbon nanotubes (CNTs) are reinforced into isotropic polymer matrix according to functional rules in which volume fractions of constituents are graded in the thickness direction. Material properties of constituents are assumed to be temperature-dependent and effective properties of nanocomposite are estimated by extended rule of mixture. Formulations are based on first-order shear deformation theory taking von Karman nonlinearity, initial geometrical imperfection, tangential constraints of edges, and two-parameter elastic foundation into consideration. Approximate solutions are assumed to satisfy simply supported boundary conditions and Galerkin method is applied to derive nonlinear temperature–deflection relations from which buckling temperatures and postbuckling equilibrium paths are determined by an iteration algorithm. Novel findings of the present study are that deteriorative influences of temperature-dependent properties on the postbuckling behavior become more serious as plate edges are partially movable, CNT volume fraction is higher, elastic foundations are stiffer, plates are thicker, and/or temperature linearly changed across the thickness.

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“…By placing the solutions (32)(33)(34) into the equations (40,41) and then putting the resulting expressions into equation 31, the average end-shortening displacements are obtained as…”

Section: Formulationsmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

Thermal postbuckling of shear deformable CNT-reinforced composite plates with tangentially restrained edges and temperature-dependent properties

Tung

Trang

2018

Journal of Thermoplastic Composite Materials

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“…Damage is not seen due to local crack propagation. Fiber damage occurs through the formation of different damage mechanisms like matrix damage and delamination [11][12][13][14] . The most common types of damage observed during honeycomb sandwich composite production are "malformation and adhesive failures" 15 .…”

Section: Introductionmentioning

confidence: 99%

The Flexural Fatigue Behavior of Honeycomb Sandwich Composites Following Low-Velocity Impacts

Solmaz¹,

Topkaya

2020

Preprint

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This study experimentally investigated the flexural fatigue behaviors of honeycomb sandwich composites subjected to low velocity impact damage by considering the type and thickness of the face sheet material, the cell size and the core height parameters. First, the static strength of undamaged specimens was determined by three-point bending loads, and calculating their fatigue lives; secondly, the fatigue lives of the specimens damaged by low velocity impact tests were then determined. Increasing the face sheet thickness and core height increased the flexural strength, while increasing the cell size decreased the flexural strength. Low velocity impact damage decreased the flexural strength and fatigue lives but increased the damping ratio for all specimens.

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“…Based on some various shear deformation theories, Arani and coauthors 15–18 dealt with problems relating to static, vibration and buckling responses of CNTRC structures in single layer and sandwich forms. Employing some various theories and methods, Kolahchi and his coworkers 19–27 investigated the dynamic instability of single-walled CNTs and the dynamic buckling of nanocomposite plates taking agglomeration and viscosity effects into consideration.…”

Section: Introductionmentioning

confidence: 99%

Thermomechanical nonlinear stability of pressure-loaded functionally graded carbon nanotube-reinforced composite doubly curved panels with tangentially restrained edges

Trang

Tung

2019

Proceedings of the Institution of Mechanical Engineers, Part C:

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Geometrically nonlinear response of doubly curved panels reinforced by carbon nanotubes exposed to thermal environments and subjected to uniform external pressure are presented in this paper. Carbon nanotubes are reinforced into isotropic matrix through uniform and functionally graded distributions. Material properties of constituents are assumed to be temperature dependent, and effective elastic moduli of carbon nanotube-reinforced composite are determined according to an extended rule of mixture. Basic equations for carbon nanotube-reinforced composite doubly curved panels are established within the framework of first-order shear deformation theory. Analytical solutions are assumed, and Galerkin method is used to derive closed-form expressions of nonlinear load–deflection relation. Separate and combined effects of carbon nanotube distribution and volume fraction, elasticity of in-plane constraint, elevated temperature, initial imperfection, geometrical ratios and stiffness of elastic foundations on the nonlinear stability of nanocomposite doubly curved panels are analyzed through numerical examples.

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Agglomeration effects on the dynamic buckling of viscoelastic microplates reinforced with SWCNTs using Bolotin method

Cited by 28 publications

References 31 publications

Thermal postbuckling of shear deformable CNT-reinforced composite plates with tangentially restrained edges and temperature-dependent properties

Thermal postbuckling of shear deformable CNT-reinforced composite plates with tangentially restrained edges and temperature-dependent properties

The Flexural Fatigue Behavior of Honeycomb Sandwich Composites Following Low-Velocity Impacts

Thermomechanical nonlinear stability of pressure-loaded functionally graded carbon nanotube-reinforced composite doubly curved panels with tangentially restrained edges

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