Ćetković, Marina

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  • Ćetković, Marina (49)

Author's Bibliography

Thermo-mechanical stability of FRP and FGM plates with geometrical imperfections using layer wise finite element

Ćetković, Marina

(2023)

TY  - GEN
AU  - Ćetković, Marina
PY  - 2023
UR  - http://www.cmseconf.org/Speaker
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/3327
AB  - One of the ultimate limit state important for the safe design of structures is failure due to buckling. The origin of buckling, as the sudden change in shape of structural component, may arise from mechanical as well from thermal loading conditions. Apart from the loading conditions, the geometrical imperfections are another parameter important for the overall structural stability. In wish to fulfil the lack of thermo-mechanical stability solutions based on Layer Wise (LW) plate theories, which will be able to include general form of geometrical imperfection, this study presents the LW finite element for thermo-mechanical stability of geometrically imperfect FRP (Fibre reinforced polymer) and FGM (Functionally Graded Material) plates. The mathematical model, based on Layer wise theory of Reddy, assumes layer wise variation of in plane displacements and constant transverse displacement through the thickness, non-linear strain displacement relations and isotropic/orthotropic material properties. The material properties of FGM plates are assumed to be constant in xy-plane and vary through the thickness by a power law function in terms of the volume fraction of the constituents. The Koiter’s model for initial geometric imperfection is adopted. The principle of virtual displacement (PVD) is utilized to derive Euler-Lagrange differential equation of linearized buckling problem. The weak form is discretized using nine node Lagrangian isoparametric finite element. The original MATLAB computer program is coded for the finite element solution and used to study influence of plate thickness a/h, aspect ratio a/b, power low index, imperfection form and material properties on thermo-mechanical stability of FRP and FGM plates. The results are compared with the one from the literature.
T2  - The 12th Global Conference on Materials Science and Engineering (CMSE 2023)
T1  - Thermo-mechanical stability of FRP and FGM plates with geometrical imperfections using layer wise finite element
UR  - https://hdl.handle.net/21.15107/rcub_grafar_3327
ER  - 
@misc{
author = "Ćetković, Marina",
year = "2023",
abstract = "One of the ultimate limit state important for the safe design of structures is failure due to buckling. The origin of buckling, as the sudden change in shape of structural component, may arise from mechanical as well from thermal loading conditions. Apart from the loading conditions, the geometrical imperfections are another parameter important for the overall structural stability. In wish to fulfil the lack of thermo-mechanical stability solutions based on Layer Wise (LW) plate theories, which will be able to include general form of geometrical imperfection, this study presents the LW finite element for thermo-mechanical stability of geometrically imperfect FRP (Fibre reinforced polymer) and FGM (Functionally Graded Material) plates. The mathematical model, based on Layer wise theory of Reddy, assumes layer wise variation of in plane displacements and constant transverse displacement through the thickness, non-linear strain displacement relations and isotropic/orthotropic material properties. The material properties of FGM plates are assumed to be constant in xy-plane and vary through the thickness by a power law function in terms of the volume fraction of the constituents. The Koiter’s model for initial geometric imperfection is adopted. The principle of virtual displacement (PVD) is utilized to derive Euler-Lagrange differential equation of linearized buckling problem. The weak form is discretized using nine node Lagrangian isoparametric finite element. The original MATLAB computer program is coded for the finite element solution and used to study influence of plate thickness a/h, aspect ratio a/b, power low index, imperfection form and material properties on thermo-mechanical stability of FRP and FGM plates. The results are compared with the one from the literature.",
journal = "The 12th Global Conference on Materials Science and Engineering (CMSE 2023)",
title = "Thermo-mechanical stability of FRP and FGM plates with geometrical imperfections using layer wise finite element",
url = "https://hdl.handle.net/21.15107/rcub_grafar_3327"
}
Ćetković, M.. (2023). Thermo-mechanical stability of FRP and FGM plates with geometrical imperfections using layer wise finite element. in The 12th Global Conference on Materials Science and Engineering (CMSE 2023).
https://hdl.handle.net/21.15107/rcub_grafar_3327
Ćetković M. Thermo-mechanical stability of FRP and FGM plates with geometrical imperfections using layer wise finite element. in The 12th Global Conference on Materials Science and Engineering (CMSE 2023). 2023;.
https://hdl.handle.net/21.15107/rcub_grafar_3327 .
Ćetković, Marina, "Thermo-mechanical stability of FRP and FGM plates with geometrical imperfections using layer wise finite element" in The 12th Global Conference on Materials Science and Engineering (CMSE 2023) (2023),
https://hdl.handle.net/21.15107/rcub_grafar_3327 .

Stability analysis of FGM plates by using layer wise displacement model

Ćetković, Marina

(Serbian Society for Computational Mechanics, 2023)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2023
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/3325
AB  - In this paper, the stability analysis of simply supported functionally graded material (FGM) plate under mechanical in–plane compressive loads is analyzed. The displacement model based on Generalized Laminate Plate Theory (GLPT) assumes piece–wise linear variation of in–plane displacements, constant transverse displacement, non–linear strain–displacement relations (in von Karman sense) and linear material properties. The properties of FGMs are assumed to be constant in xy–plane and vary through thickness by a power law function in terms of volume fraction of the constituents. The mathematical model includes the quadratic variation of transverse shear stresses within each layer of the plate. The principle of virtual displacements (PVD) is used to derive Euler–Lagrange differential equations of linearized buckling problem. Closed form solution is derived following the Navier’s technique and solving the eigenvalue problem. The original MATLAB computer program is coded for the numerical solution. The results reveal that the effects of side–to–thickness ratio, power–low index and modulus ratio have significant effect on critical buckling loads of FGM plates.
PB  - Serbian Society for Computational Mechanics
C3  - 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia
T1  - Stability analysis of FGM plates by using layer wise displacement model
EP  - 10
SP  - 1
UR  - https://hdl.handle.net/21.15107/rcub_grafar_3325
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2023",
abstract = "In this paper, the stability analysis of simply supported functionally graded material (FGM) plate under mechanical in–plane compressive loads is analyzed. The displacement model based on Generalized Laminate Plate Theory (GLPT) assumes piece–wise linear variation of in–plane displacements, constant transverse displacement, non–linear strain–displacement relations (in von Karman sense) and linear material properties. The properties of FGMs are assumed to be constant in xy–plane and vary through thickness by a power law function in terms of volume fraction of the constituents. The mathematical model includes the quadratic variation of transverse shear stresses within each layer of the plate. The principle of virtual displacements (PVD) is used to derive Euler–Lagrange differential equations of linearized buckling problem. Closed form solution is derived following the Navier’s technique and solving the eigenvalue problem. The original MATLAB computer program is coded for the numerical solution. The results reveal that the effects of side–to–thickness ratio, power–low index and modulus ratio have significant effect on critical buckling loads of FGM plates.",
publisher = "Serbian Society for Computational Mechanics",
journal = "9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia",
title = "Stability analysis of FGM plates by using layer wise displacement model",
pages = "10-1",
url = "https://hdl.handle.net/21.15107/rcub_grafar_3325"
}
Ćetković, M.. (2023). Stability analysis of FGM plates by using layer wise displacement model. in 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia
Serbian Society for Computational Mechanics., 1-10.
https://hdl.handle.net/21.15107/rcub_grafar_3325
Ćetković M. Stability analysis of FGM plates by using layer wise displacement model. in 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia. 2023;:1-10.
https://hdl.handle.net/21.15107/rcub_grafar_3325 .
Ćetković, Marina, "Stability analysis of FGM plates by using layer wise displacement model" in 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia (2023):1-10,
https://hdl.handle.net/21.15107/rcub_grafar_3325 .

Free vibration analysis of FGM plates by using layer wise displacement model

Ćetković, Marina

(Serbian Society for Computational Mechanics, 2023)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2023
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/3326
AB  - In this paper, the free vibration analysis of simply supported functionally graded material (FGM) plate is analyzed. The displacement model based on Generalized Laminate Plate Theory (GLPT) assumes layer wise (LW) linear variation of in–plane displacements, constant transverse displacement, linear strain–displacement relations and linear material properties. The effective material properties of FGMs are assumed to be given by the Voigt’s rule of mixture (ROM). The Power law distribution of volume fraction is assumed through the plate thickness. The mathematical model includes the quadratic variation of transverse shear stresses within each mathematical layer of the plate. The principle of virtual displacements (PVD) is used to derive Euler–Lagrange differential equations of motions for free vibration problem. The Closed form solution is derived following the Navier’s technique and solving the eigenvalue problem. An original MATLAB computer program is coded for the numerical solution. The results reveal that the effects of side–to–thickness ratio, power–low index and material properties have significant effect on free vibration frequencies of FGM plates.
PB  - Serbian Society for Computational Mechanics
C3  - 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia
T1  - Free vibration analysis of FGM plates by using layer wise displacement model
UR  - https://hdl.handle.net/21.15107/rcub_grafar_3326
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2023",
abstract = "In this paper, the free vibration analysis of simply supported functionally graded material (FGM) plate is analyzed. The displacement model based on Generalized Laminate Plate Theory (GLPT) assumes layer wise (LW) linear variation of in–plane displacements, constant transverse displacement, linear strain–displacement relations and linear material properties. The effective material properties of FGMs are assumed to be given by the Voigt’s rule of mixture (ROM). The Power law distribution of volume fraction is assumed through the plate thickness. The mathematical model includes the quadratic variation of transverse shear stresses within each mathematical layer of the plate. The principle of virtual displacements (PVD) is used to derive Euler–Lagrange differential equations of motions for free vibration problem. The Closed form solution is derived following the Navier’s technique and solving the eigenvalue problem. An original MATLAB computer program is coded for the numerical solution. The results reveal that the effects of side–to–thickness ratio, power–low index and material properties have significant effect on free vibration frequencies of FGM plates.",
publisher = "Serbian Society for Computational Mechanics",
journal = "9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia",
title = "Free vibration analysis of FGM plates by using layer wise displacement model",
url = "https://hdl.handle.net/21.15107/rcub_grafar_3326"
}
Ćetković, M.. (2023). Free vibration analysis of FGM plates by using layer wise displacement model. in 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia
Serbian Society for Computational Mechanics..
https://hdl.handle.net/21.15107/rcub_grafar_3326
Ćetković M. Free vibration analysis of FGM plates by using layer wise displacement model. in 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia. 2023;.
https://hdl.handle.net/21.15107/rcub_grafar_3326 .
Ćetković, Marina, "Free vibration analysis of FGM plates by using layer wise displacement model" in 9th International Congress of the Serbian Society of Mechanics, July 5–7, 2023, Vrnjačka Banja, Serbia (2023),
https://hdl.handle.net/21.15107/rcub_grafar_3326 .

Free vibrations of FGM plates with imperfections using layerwise finite element

Ćetković, Marina

(Mathematical Institute SANU, Belgrade, Serbia, 2022)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2022
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/2695
AB  - The initial geometrical imperfections, as deviations between the actual and intended shape, are in most cases randomly distributed in real structures and their real shape is not known in advance. Most of the studies reported up to date are based on simplified assumption that the initial geometric imperfection has a similar form to the deformed shape of the plate or sinusoidal form. Moreover, most of the mentioned studies present the analytical solutions for imperfect plates, restricred to simply supported boundary conditions. In wish to fulfil the lack of free vibration solutions based on Layer Wise (LW) plate theories, which will be able to include general form of geometrical imperfection and arbitrary boundary conditions, in this study a LW finite element solution is presented for free vibrations of geometrically imperfect FGM (Functionally Graded Material)  plates.
After establishing the accuracy of the present layer wise model for linear and geometrically nonlinear bending, vibration and buckling analysis of laminated composite and sandwich plates subjected to mechanical load, as well as for thermal bending and buckling of laminated composite and sandwich plates, in this paper, free vibration of geometrically imperfect FGM plates is presented. The mathematical model, based on Layer wise theory of Reddy, assumes layer wise variation of in plane displacements and constant transverse displacement through the thickness, linear strain displacement relations and isotropic/orthotropic material properties. The material properties of FGM plates are assumed to be constant in xy-plane and vary through the thickness by a power law function in terms of the volume fraction of the constituents. The effective materials properties are given by the rule of mixture. The Koiter’s model for initial geometric imperfection is adopted. In order to include various possible imperfection modes, such as sine type, local type and global type, an imperfection function in the form of the product of trigonometric function and hyperbolic function in (x,y) plane is used. The principle of virtual displacement (PVD) is used to derive Euler-Lagrange differential equation of motion. The weak form is discretized using nine node Lagrangian isoparametric finite element. The original MATLAB computer program is coded for the finite element solution. The effects of imperfection mode and amplitude on fundamental frequencies is analysed. The accuracy of the numerical model is verified by comparison with the available results from the literature. It is found that geometric imperfection greatly affect the free vibration behaviour of FGM plates and should be taken into account when designing safe and functional structures.
PB  - Mathematical Institute SANU, Belgrade, Serbia
C3  - 1st International Conference on Mathematical Modelling in Mechanics and Engineering (ICME2022)
T1  - Free vibrations of FGM plates with imperfections using layerwise finite element
UR  - https://hdl.handle.net/21.15107/rcub_grafar_2695
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2022",
abstract = "The initial geometrical imperfections, as deviations between the actual and intended shape, are in most cases randomly distributed in real structures and their real shape is not known in advance. Most of the studies reported up to date are based on simplified assumption that the initial geometric imperfection has a similar form to the deformed shape of the plate or sinusoidal form. Moreover, most of the mentioned studies present the analytical solutions for imperfect plates, restricred to simply supported boundary conditions. In wish to fulfil the lack of free vibration solutions based on Layer Wise (LW) plate theories, which will be able to include general form of geometrical imperfection and arbitrary boundary conditions, in this study a LW finite element solution is presented for free vibrations of geometrically imperfect FGM (Functionally Graded Material)  plates.
After establishing the accuracy of the present layer wise model for linear and geometrically nonlinear bending, vibration and buckling analysis of laminated composite and sandwich plates subjected to mechanical load, as well as for thermal bending and buckling of laminated composite and sandwich plates, in this paper, free vibration of geometrically imperfect FGM plates is presented. The mathematical model, based on Layer wise theory of Reddy, assumes layer wise variation of in plane displacements and constant transverse displacement through the thickness, linear strain displacement relations and isotropic/orthotropic material properties. The material properties of FGM plates are assumed to be constant in xy-plane and vary through the thickness by a power law function in terms of the volume fraction of the constituents. The effective materials properties are given by the rule of mixture. The Koiter’s model for initial geometric imperfection is adopted. In order to include various possible imperfection modes, such as sine type, local type and global type, an imperfection function in the form of the product of trigonometric function and hyperbolic function in (x,y) plane is used. The principle of virtual displacement (PVD) is used to derive Euler-Lagrange differential equation of motion. The weak form is discretized using nine node Lagrangian isoparametric finite element. The original MATLAB computer program is coded for the finite element solution. The effects of imperfection mode and amplitude on fundamental frequencies is analysed. The accuracy of the numerical model is verified by comparison with the available results from the literature. It is found that geometric imperfection greatly affect the free vibration behaviour of FGM plates and should be taken into account when designing safe and functional structures.",
publisher = "Mathematical Institute SANU, Belgrade, Serbia",
journal = "1st International Conference on Mathematical Modelling in Mechanics and Engineering (ICME2022)",
title = "Free vibrations of FGM plates with imperfections using layerwise finite element",
url = "https://hdl.handle.net/21.15107/rcub_grafar_2695"
}
Ćetković, M.. (2022). Free vibrations of FGM plates with imperfections using layerwise finite element. in 1st International Conference on Mathematical Modelling in Mechanics and Engineering (ICME2022)
Mathematical Institute SANU, Belgrade, Serbia..
https://hdl.handle.net/21.15107/rcub_grafar_2695
Ćetković M. Free vibrations of FGM plates with imperfections using layerwise finite element. in 1st International Conference on Mathematical Modelling in Mechanics and Engineering (ICME2022). 2022;.
https://hdl.handle.net/21.15107/rcub_grafar_2695 .
Ćetković, Marina, "Free vibrations of FGM plates with imperfections using layerwise finite element" in 1st International Conference on Mathematical Modelling in Mechanics and Engineering (ICME2022) (2022),
https://hdl.handle.net/21.15107/rcub_grafar_2695 .

Thermal Buckling of Laminated Composite and FGM plates with Imperfection using Layerwise Finite Element

Ćetković, Marina

(THE SCIENTISTT India, 2022)

TY  - GEN
AU  - Ćetković, Marina
PY  - 2022
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/2686
PB  - THE SCIENTISTT India
T2  - 2nd Global Summit on Civil, Architectural and Environmental Engineering (GSCAEE2022)
T1  - Thermal Buckling of Laminated Composite and FGM plates with Imperfection using Layerwise Finite Element
UR  - https://hdl.handle.net/21.15107/rcub_grafar_2686
ER  - 
@misc{
author = "Ćetković, Marina",
year = "2022",
publisher = "THE SCIENTISTT India",
journal = "2nd Global Summit on Civil, Architectural and Environmental Engineering (GSCAEE2022)",
title = "Thermal Buckling of Laminated Composite and FGM plates with Imperfection using Layerwise Finite Element",
url = "https://hdl.handle.net/21.15107/rcub_grafar_2686"
}
Ćetković, M.. (2022). Thermal Buckling of Laminated Composite and FGM plates with Imperfection using Layerwise Finite Element. in 2nd Global Summit on Civil, Architectural and Environmental Engineering (GSCAEE2022)
THE SCIENTISTT India..
https://hdl.handle.net/21.15107/rcub_grafar_2686
Ćetković M. Thermal Buckling of Laminated Composite and FGM plates with Imperfection using Layerwise Finite Element. in 2nd Global Summit on Civil, Architectural and Environmental Engineering (GSCAEE2022). 2022;.
https://hdl.handle.net/21.15107/rcub_grafar_2686 .
Ćetković, Marina, "Thermal Buckling of Laminated Composite and FGM plates with Imperfection using Layerwise Finite Element" in 2nd Global Summit on Civil, Architectural and Environmental Engineering (GSCAEE2022) (2022),
https://hdl.handle.net/21.15107/rcub_grafar_2686 .

Influence of initial geometrical imperfections on thermal stability of laminated composite plates using layerwise finite element

Ćetković, Marina

(www.elsevier.com/locate/compstruct, 2022)

TY  - JOUR
AU  - Ćetković, Marina
PY  - 2022
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/2660
AB  - In this paper, the influence of initial geometrical imperfections on thermal stability of laminated composite plates using Layer wise plate model is presented. The mathematical model assumes layer wise variation of in-plane displacements, non-linear strain-displacement relations (in von Karman sense) and linear thermo mechanical material properties. The Koiter’s model for initial geometrical imperfection is adopted. Principle of virtual displacements (PVD) is used to derive Euler-Lagrange differential equations of linearized buckling problem. The weak form is discretized using nine-node Lagrangian isoparametric finite element. The original MATLAB program is coded for finite element solution. The effects of imperfection mode and amplitude, temperature distribution, side to thickness ratio b/h, aspect ratio b/a, boundary conditions and lamination scheme on critical buckling temperature are analysed. The accuracy of the numerical model is verified by comparison with the available results from the literature and new results are presented.
PB  - www.elsevier.com/locate/compstruct
T2  - Composite Structures
T1  - Influence of initial geometrical imperfections on thermal stability of laminated composite plates using layerwise finite element
VL  - 291
DO  - 10.1016/j.compstruct.2022.115547
ER  - 
@article{
author = "Ćetković, Marina",
year = "2022",
abstract = "In this paper, the influence of initial geometrical imperfections on thermal stability of laminated composite plates using Layer wise plate model is presented. The mathematical model assumes layer wise variation of in-plane displacements, non-linear strain-displacement relations (in von Karman sense) and linear thermo mechanical material properties. The Koiter’s model for initial geometrical imperfection is adopted. Principle of virtual displacements (PVD) is used to derive Euler-Lagrange differential equations of linearized buckling problem. The weak form is discretized using nine-node Lagrangian isoparametric finite element. The original MATLAB program is coded for finite element solution. The effects of imperfection mode and amplitude, temperature distribution, side to thickness ratio b/h, aspect ratio b/a, boundary conditions and lamination scheme on critical buckling temperature are analysed. The accuracy of the numerical model is verified by comparison with the available results from the literature and new results are presented.",
publisher = "www.elsevier.com/locate/compstruct",
journal = "Composite Structures",
title = "Influence of initial geometrical imperfections on thermal stability of laminated composite plates using layerwise finite element",
volume = "291",
doi = "10.1016/j.compstruct.2022.115547"
}
Ćetković, M.. (2022). Influence of initial geometrical imperfections on thermal stability of laminated composite plates using layerwise finite element. in Composite Structures
www.elsevier.com/locate/compstruct., 291.
https://doi.org/10.1016/j.compstruct.2022.115547
Ćetković M. Influence of initial geometrical imperfections on thermal stability of laminated composite plates using layerwise finite element. in Composite Structures. 2022;291.
doi:10.1016/j.compstruct.2022.115547 .
Ćetković, Marina, "Influence of initial geometrical imperfections on thermal stability of laminated composite plates using layerwise finite element" in Composite Structures, 291 (2022),
https://doi.org/10.1016/j.compstruct.2022.115547 . .
8

Layerwise finite element for free vibration of geometricaly imperfect composite plates

Ćetković, Marina

(UNIVERSITY OF MONTENEGRO FACULTY OF CIVIL ENGINEERING, 2022)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2022
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/2642
AB  - After establishing the accuracy of the present layerwise model for linear and geometrically nonlinear bending, vibration and buckling analysis of laminated composite and sandwich plates subjected to mechanical load, as well as for thermal bending and buckling of laminated composite and sandwich plates, in this paper, free vibration of geometrically imperfect composite plate is presented. The mathematical model, based on Layerwise theory of Reddy, assumes layerwise variation of in plane displacements and constant transverse displacement through the thickness, linear strain displacement relations and linear orthotropic material properties. The Koiter’s model for initial geometric imperfection is adopted. In order to include various possible imperfection modes, such as sine type, local type and global type, an imperfection function in the form of the product of trigonometric function and hyperbolic function in (x,y) plane is used. The principle of virtual displacement (PVD) is used to derive Euler-Lagrange differential equation of motion. The weak form is discretized using nine node Lagrangian isoparametric finite element. Element stiffness matrix, initial stiffness matrix and element mass matrix are evaluated using 3x3 Gauss-Legendre integration scheme, for 2D quadratic in-plane interpolation. Consistent element mass matrix is implemented in order to preserve the total mass of the element. The original MATLAB computer program is coded for the finite element solution. The effects of imperfection amplitude on fundamental frequencies is analysed. The accuracy of the numerical model is verified by comparison with the available results from the literature. It is found that geometric imperfection greatly affect the free vibration behaviour of composite laminates and should be taken into account when designing safe and functional structures.
PB  - UNIVERSITY OF MONTENEGRO FACULTY OF CIVIL ENGINEERING
C3  - THE EIGHTH INTERNATIONAL CONFERENCE CIVIL ENGINEERING SCIENCE & PRACTICE
T1  - Layerwise finite element for free vibration of geometricaly imperfect composite plates
EP  - 134
SP  - 127
UR  - https://hdl.handle.net/21.15107/rcub_grafar_2642
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2022",
abstract = "After establishing the accuracy of the present layerwise model for linear and geometrically nonlinear bending, vibration and buckling analysis of laminated composite and sandwich plates subjected to mechanical load, as well as for thermal bending and buckling of laminated composite and sandwich plates, in this paper, free vibration of geometrically imperfect composite plate is presented. The mathematical model, based on Layerwise theory of Reddy, assumes layerwise variation of in plane displacements and constant transverse displacement through the thickness, linear strain displacement relations and linear orthotropic material properties. The Koiter’s model for initial geometric imperfection is adopted. In order to include various possible imperfection modes, such as sine type, local type and global type, an imperfection function in the form of the product of trigonometric function and hyperbolic function in (x,y) plane is used. The principle of virtual displacement (PVD) is used to derive Euler-Lagrange differential equation of motion. The weak form is discretized using nine node Lagrangian isoparametric finite element. Element stiffness matrix, initial stiffness matrix and element mass matrix are evaluated using 3x3 Gauss-Legendre integration scheme, for 2D quadratic in-plane interpolation. Consistent element mass matrix is implemented in order to preserve the total mass of the element. The original MATLAB computer program is coded for the finite element solution. The effects of imperfection amplitude on fundamental frequencies is analysed. The accuracy of the numerical model is verified by comparison with the available results from the literature. It is found that geometric imperfection greatly affect the free vibration behaviour of composite laminates and should be taken into account when designing safe and functional structures.",
publisher = "UNIVERSITY OF MONTENEGRO FACULTY OF CIVIL ENGINEERING",
journal = "THE EIGHTH INTERNATIONAL CONFERENCE CIVIL ENGINEERING SCIENCE & PRACTICE",
title = "Layerwise finite element for free vibration of geometricaly imperfect composite plates",
pages = "134-127",
url = "https://hdl.handle.net/21.15107/rcub_grafar_2642"
}
Ćetković, M.. (2022). Layerwise finite element for free vibration of geometricaly imperfect composite plates. in THE EIGHTH INTERNATIONAL CONFERENCE CIVIL ENGINEERING SCIENCE & PRACTICE
UNIVERSITY OF MONTENEGRO FACULTY OF CIVIL ENGINEERING., 127-134.
https://hdl.handle.net/21.15107/rcub_grafar_2642
Ćetković M. Layerwise finite element for free vibration of geometricaly imperfect composite plates. in THE EIGHTH INTERNATIONAL CONFERENCE CIVIL ENGINEERING SCIENCE & PRACTICE. 2022;:127-134.
https://hdl.handle.net/21.15107/rcub_grafar_2642 .
Ćetković, Marina, "Layerwise finite element for free vibration of geometricaly imperfect composite plates" in THE EIGHTH INTERNATIONAL CONFERENCE CIVIL ENGINEERING SCIENCE & PRACTICE (2022):127-134,
https://hdl.handle.net/21.15107/rcub_grafar_2642 .

Nonlinear analysis of composite plates using layerwise finite element

Ćetković, Marina

(Mathematical Institute of the Serbian Academy of Sciences and Arts National Institute of the Republic of Serbia, 2019)

TY  - GEN
AU  - Ćetković, Marina
PY  - 2019
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/2687
PB  - Mathematical Institute of the Serbian Academy of Sciences and Arts National Institute of the Republic of Serbia
T2  - Mechanics of machines and Mechanisms-Models and mathematical Methods
T1  - Nonlinear analysis of composite plates using layerwise finite element
UR  - https://hdl.handle.net/21.15107/rcub_grafar_2687
ER  - 
@misc{
author = "Ćetković, Marina",
year = "2019",
publisher = "Mathematical Institute of the Serbian Academy of Sciences and Arts National Institute of the Republic of Serbia",
journal = "Mechanics of machines and Mechanisms-Models and mathematical Methods",
title = "Nonlinear analysis of composite plates using layerwise finite element",
url = "https://hdl.handle.net/21.15107/rcub_grafar_2687"
}
Ćetković, M.. (2019). Nonlinear analysis of composite plates using layerwise finite element. in Mechanics of machines and Mechanisms-Models and mathematical Methods
Mathematical Institute of the Serbian Academy of Sciences and Arts National Institute of the Republic of Serbia..
https://hdl.handle.net/21.15107/rcub_grafar_2687
Ćetković M. Nonlinear analysis of composite plates using layerwise finite element. in Mechanics of machines and Mechanisms-Models and mathematical Methods. 2019;.
https://hdl.handle.net/21.15107/rcub_grafar_2687 .
Ćetković, Marina, "Nonlinear analysis of composite plates using layerwise finite element" in Mechanics of machines and Mechanisms-Models and mathematical Methods (2019),
https://hdl.handle.net/21.15107/rcub_grafar_2687 .

Finite Element Model of Imperfect Plate in Thermal Environment

Ćetković, Marina

(Serbian Society of Mechanics, Belgrade, 2019, 2019)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2019
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1886
AB  - In this paper a finite element model for thermal buckling of imperfect plates using Layer Wise (LW) plate mode [1] is presented. The model assumes layerwise variation of in-plane displacements and constant transverse displacement through the thickness of the plate, non-linear strain-displacement relations (in von Karman sense) and linear thermo mechanical material properties. The Koiter model for imperfection is adopted. The Principle of virtual displacements (PVD) is used to derive the weak form of linearized buckling problem. The weak form is discretized using Lagrangian nine-node isoparametric finite element. The original MATLAB program is coded for finite element solution. The effects of imperfection amplitude, imperfection form and plate aspect ratio a/h on critical temperature are analyzed. The accuracy of the numerical model is verified by comparison with the available results from the literature.
PB  - Serbian Society of Mechanics, Belgrade, 2019
C3  - Proceedings / The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, Serbia, June 24-26, 2019
T1  - Finite Element Model of Imperfect Plate in Thermal Environment
EP  - 10
SP  - 1
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1886
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2019",
abstract = "In this paper a finite element model for thermal buckling of imperfect plates using Layer Wise (LW) plate mode [1] is presented. The model assumes layerwise variation of in-plane displacements and constant transverse displacement through the thickness of the plate, non-linear strain-displacement relations (in von Karman sense) and linear thermo mechanical material properties. The Koiter model for imperfection is adopted. The Principle of virtual displacements (PVD) is used to derive the weak form of linearized buckling problem. The weak form is discretized using Lagrangian nine-node isoparametric finite element. The original MATLAB program is coded for finite element solution. The effects of imperfection amplitude, imperfection form and plate aspect ratio a/h on critical temperature are analyzed. The accuracy of the numerical model is verified by comparison with the available results from the literature.",
publisher = "Serbian Society of Mechanics, Belgrade, 2019",
journal = "Proceedings / The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, Serbia, June 24-26, 2019",
title = "Finite Element Model of Imperfect Plate in Thermal Environment",
pages = "10-1",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1886"
}
Ćetković, M.. (2019). Finite Element Model of Imperfect Plate in Thermal Environment. in Proceedings / The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, Serbia, June 24-26, 2019
Serbian Society of Mechanics, Belgrade, 2019., 1-10.
https://hdl.handle.net/21.15107/rcub_grafar_1886
Ćetković M. Finite Element Model of Imperfect Plate in Thermal Environment. in Proceedings / The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, Serbia, June 24-26, 2019. 2019;:1-10.
https://hdl.handle.net/21.15107/rcub_grafar_1886 .
Ćetković, Marina, "Finite Element Model of Imperfect Plate in Thermal Environment" in Proceedings / The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, Serbia, June 24-26, 2019 (2019):1-10,
https://hdl.handle.net/21.15107/rcub_grafar_1886 .

Nonlinear Analysis of Composite Plates using Continuum Finite Element

Ćetković, Marina

(University of Belgrade, Faculty of Civil Engineering, 2019)

TY  - CHAP
AU  - Ćetković, Marina
PY  - 2019
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1872
AB  - In this paper the geometrically nonlinear plate finite element model, hitherto not reported in the literature, is developed using the total Lagrange formulation. With the layer wise displacement field of Reddy [1], nonlinear Green-Lagrange small strain large displacements relations (in the von Karman sense) and linear elastic orthotropic material properties for each lamina, the 3D elasticity equations are reduced to 2D problem and the nonlinear equilibrium integral form is obtained. By performing the linearization on nonlinear integral form and then the discretization on linearized integral form, tangent stiffness matrix is obtained with less manipulation and in more consistent form, compared to the one obtained using laminated element approach from literature [8]. Symmetric tangent stiffness matrixes, together with internal force vector are then utilized in Newton Raphson’s method for the numerical solution of nonlinear incremental finite element equilibrium equations. The originally coded MATLAB computer program for the finite element solution is used to verify the accuracy of the numerical model, by calculating nonlinear response of plates with different mechanical properties, which are isotropic, orthotropic and anisotropic (cross ply and angle ply), different plate thickness, different boundary conditions and different load direction (unloading/loading). The obtained results are compared with available results from the literature and the linear solutions from the author’s previous papers.
AB  - У раду је по први пут у литературу формулисан геометријски нелинеаран коначни елемент плоче заснован на  тоталној Lagrange-овој формулацији. Користећи слојевиту теорију плоча Reddy-a [1], нелинеарне Green-Lagrange-ове везе деформација и померања (у von Karman-овом смислу) и линеарнo еластичне ортотропне карактеристике за сваки слој, 3Д једначине еластичности су редуковане на 2Д проблем и добијена је нелинеарна интегрална форма. Пошто је спроведена линеаризација на нелинеарној интегралној форми, а потом и дискретизација, добијена је тангентна матрица крутости коначног елемента и то са мање математичких операција, у поређењу са оном добијеном у случају ламинатног коначног елемента из литературе [8]. Симетрична тангентна матрица крутости, заједно са вектором унутрашњих чворних сила, примењени су у Newton Raphson-овој методи за решавање нелинеарних инкременталних једначина равнотеже. За решење по МКЕ написан је оригинални програм у MATLAB програмском језику. Програмом су анализиране плоче различитих механичких карактеристика, односно изотропне, ортотропне и ламинатне (cross ply и angle ply), различитих дебљина, различитих граничних услова и различитих режима оптерећења/растерећења. Добијена решења су упоређена са решењима из литературе и изведени су закључци.
PB  - University of Belgrade, Faculty of Civil Engineering
PB  - University of Montenegro, Faculty of Civil Engineering
PB  - Academy of Engineering Sciences of Seribia
T2  - Theory of Civil Engineering Structures─Monograph dedicated to the memory of Professor Miodrag Sekulović
T1  - Nonlinear Analysis of Composite Plates using Continuum Finite Element
T1  - Нелинеарна анализа композитних плоча применом коначног елемента континуума
EP  - 112
SP  - 101
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1872
ER  - 
@inbook{
author = "Ćetković, Marina",
year = "2019",
abstract = "In this paper the geometrically nonlinear plate finite element model, hitherto not reported in the literature, is developed using the total Lagrange formulation. With the layer wise displacement field of Reddy [1], nonlinear Green-Lagrange small strain large displacements relations (in the von Karman sense) and linear elastic orthotropic material properties for each lamina, the 3D elasticity equations are reduced to 2D problem and the nonlinear equilibrium integral form is obtained. By performing the linearization on nonlinear integral form and then the discretization on linearized integral form, tangent stiffness matrix is obtained with less manipulation and in more consistent form, compared to the one obtained using laminated element approach from literature [8]. Symmetric tangent stiffness matrixes, together with internal force vector are then utilized in Newton Raphson’s method for the numerical solution of nonlinear incremental finite element equilibrium equations. The originally coded MATLAB computer program for the finite element solution is used to verify the accuracy of the numerical model, by calculating nonlinear response of plates with different mechanical properties, which are isotropic, orthotropic and anisotropic (cross ply and angle ply), different plate thickness, different boundary conditions and different load direction (unloading/loading). The obtained results are compared with available results from the literature and the linear solutions from the author’s previous papers., У раду је по први пут у литературу формулисан геометријски нелинеаран коначни елемент плоче заснован на  тоталној Lagrange-овој формулацији. Користећи слојевиту теорију плоча Reddy-a [1], нелинеарне Green-Lagrange-ове везе деформација и померања (у von Karman-овом смислу) и линеарнo еластичне ортотропне карактеристике за сваки слој, 3Д једначине еластичности су редуковане на 2Д проблем и добијена је нелинеарна интегрална форма. Пошто је спроведена линеаризација на нелинеарној интегралној форми, а потом и дискретизација, добијена је тангентна матрица крутости коначног елемента и то са мање математичких операција, у поређењу са оном добијеном у случају ламинатног коначног елемента из литературе [8]. Симетрична тангентна матрица крутости, заједно са вектором унутрашњих чворних сила, примењени су у Newton Raphson-овој методи за решавање нелинеарних инкременталних једначина равнотеже. За решење по МКЕ написан је оригинални програм у MATLAB програмском језику. Програмом су анализиране плоче различитих механичких карактеристика, односно изотропне, ортотропне и ламинатне (cross ply и angle ply), различитих дебљина, различитих граничних услова и различитих режима оптерећења/растерећења. Добијена решења су упоређена са решењима из литературе и изведени су закључци.",
publisher = "University of Belgrade, Faculty of Civil Engineering, University of Montenegro, Faculty of Civil Engineering, Academy of Engineering Sciences of Seribia",
journal = "Theory of Civil Engineering Structures─Monograph dedicated to the memory of Professor Miodrag Sekulović",
booktitle = "Nonlinear Analysis of Composite Plates using Continuum Finite Element, Нелинеарна анализа композитних плоча применом коначног елемента континуума",
pages = "112-101",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1872"
}
Ćetković, M.. (2019). Nonlinear Analysis of Composite Plates using Continuum Finite Element. in Theory of Civil Engineering Structures─Monograph dedicated to the memory of Professor Miodrag Sekulović
University of Belgrade, Faculty of Civil Engineering., 101-112.
https://hdl.handle.net/21.15107/rcub_grafar_1872
Ćetković M. Nonlinear Analysis of Composite Plates using Continuum Finite Element. in Theory of Civil Engineering Structures─Monograph dedicated to the memory of Professor Miodrag Sekulović. 2019;:101-112.
https://hdl.handle.net/21.15107/rcub_grafar_1872 .
Ćetković, Marina, "Nonlinear Analysis of Composite Plates using Continuum Finite Element" in Theory of Civil Engineering Structures─Monograph dedicated to the memory of Professor Miodrag Sekulović (2019):101-112,
https://hdl.handle.net/21.15107/rcub_grafar_1872 .

Imperfection sensitivity of plates on thermal environment

Ćetković, Marina

(Serbian Society of Mechanics ; Faculty of Mechanical Engineering, University of Belgrade,Belgrade, Belgrade, 2017)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2017
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1544
AB  - In this paper a thermal buckling of imperfect plates using Layer Wise (LW) plate model [1] is presented. The model assumes layerwise variation of in-plane displacements and constant transverse displacement through the thickness of the plate, non-linear strain-displacement relations (in von Karman sense) and linear thermo mechanical material properties. The Koiter model for imperfection is adopted. Principle of virtual displacements (PVD) is used to derive Euler-Lagrange differential equations of linearized buckling problem. Euler-Lagrange differential equations are then solved using Navier's analytical solution. The original MATLAB program is coded for analytical solution. The effects of imperfection amplitude, temperature distribution, side to thickness ratio b/a and aspect ratio b/h on critical temperature are analyzed. The accuracy of the numerical model is verified by comparison with the available results from the literature.
PB  - Serbian Society of Mechanics ; Faculty of Mechanical Engineering, University of Belgrade,Belgrade, Belgrade
C3  - Proceedings / The 6th International Congress of Serbian Society of Mechanics, Tara, June 19-21, 2017
T1  - Imperfection sensitivity of plates on thermal environment
EP  - 8
SP  - 1
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1544
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2017",
abstract = "In this paper a thermal buckling of imperfect plates using Layer Wise (LW) plate model [1] is presented. The model assumes layerwise variation of in-plane displacements and constant transverse displacement through the thickness of the plate, non-linear strain-displacement relations (in von Karman sense) and linear thermo mechanical material properties. The Koiter model for imperfection is adopted. Principle of virtual displacements (PVD) is used to derive Euler-Lagrange differential equations of linearized buckling problem. Euler-Lagrange differential equations are then solved using Navier's analytical solution. The original MATLAB program is coded for analytical solution. The effects of imperfection amplitude, temperature distribution, side to thickness ratio b/a and aspect ratio b/h on critical temperature are analyzed. The accuracy of the numerical model is verified by comparison with the available results from the literature.",
publisher = "Serbian Society of Mechanics ; Faculty of Mechanical Engineering, University of Belgrade,Belgrade, Belgrade",
journal = "Proceedings / The 6th International Congress of Serbian Society of Mechanics, Tara, June 19-21, 2017",
title = "Imperfection sensitivity of plates on thermal environment",
pages = "8-1",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1544"
}
Ćetković, M.. (2017). Imperfection sensitivity of plates on thermal environment. in Proceedings / The 6th International Congress of Serbian Society of Mechanics, Tara, June 19-21, 2017
Serbian Society of Mechanics ; Faculty of Mechanical Engineering, University of Belgrade,Belgrade, Belgrade., 1-8.
https://hdl.handle.net/21.15107/rcub_grafar_1544
Ćetković M. Imperfection sensitivity of plates on thermal environment. in Proceedings / The 6th International Congress of Serbian Society of Mechanics, Tara, June 19-21, 2017. 2017;:1-8.
https://hdl.handle.net/21.15107/rcub_grafar_1544 .
Ćetković, Marina, "Imperfection sensitivity of plates on thermal environment" in Proceedings / The 6th International Congress of Serbian Society of Mechanics, Tara, June 19-21, 2017 (2017):1-8,
https://hdl.handle.net/21.15107/rcub_grafar_1544 .

Thermo-elastic Stability of Angle-ply laminates Application of Layerwise Finite Element

Ćetković, Marina; Geörgy, L.

(2016)

TY  - JOUR
AU  - Ćetković, Marina
AU  - Geörgy, L.
PY  - 2016
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1052
T2  - Structural Integrity and life
T1  - Thermo-elastic Stability of Angle-ply laminates Application of Layerwise Finite Element
EP  - 48
IS  - 1
SP  - 43
VL  - 16
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1052
ER  - 
@article{
author = "Ćetković, Marina and Geörgy, L.",
year = "2016",
journal = "Structural Integrity and life",
title = "Thermo-elastic Stability of Angle-ply laminates Application of Layerwise Finite Element",
pages = "48-43",
number = "1",
volume = "16",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1052"
}
Ćetković, M.,& Geörgy, L.. (2016). Thermo-elastic Stability of Angle-ply laminates Application of Layerwise Finite Element. in Structural Integrity and life, 16(1), 43-48.
https://hdl.handle.net/21.15107/rcub_grafar_1052
Ćetković M, Geörgy L. Thermo-elastic Stability of Angle-ply laminates Application of Layerwise Finite Element. in Structural Integrity and life. 2016;16(1):43-48.
https://hdl.handle.net/21.15107/rcub_grafar_1052 .
Ćetković, Marina, Geörgy, L., "Thermo-elastic Stability of Angle-ply laminates Application of Layerwise Finite Element" in Structural Integrity and life, 16, no. 1 (2016):43-48,
https://hdl.handle.net/21.15107/rcub_grafar_1052 .

Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates

Ćetković, Marina

(Univerzitet Crne Gore, Građevinski fakultet, Podgorica, 2016)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2016
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1500
PB  - Univerzitet Crne Gore, Građevinski fakultet, Podgorica
C3  - Zbornik radova / Šesti Internacionalni naučno-stručni skup Građevinarstvo - nauka i praksa, Žabljak, 7-11. 03. 2016.
T1  - Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates
EP  - 48
SP  - 41
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1500
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2016",
publisher = "Univerzitet Crne Gore, Građevinski fakultet, Podgorica",
journal = "Zbornik radova / Šesti Internacionalni naučno-stručni skup Građevinarstvo - nauka i praksa, Žabljak, 7-11. 03. 2016.",
title = "Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates",
pages = "48-41",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1500"
}
Ćetković, M.. (2016). Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates. in Zbornik radova / Šesti Internacionalni naučno-stručni skup Građevinarstvo - nauka i praksa, Žabljak, 7-11. 03. 2016.
Univerzitet Crne Gore, Građevinski fakultet, Podgorica., 41-48.
https://hdl.handle.net/21.15107/rcub_grafar_1500
Ćetković M. Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates. in Zbornik radova / Šesti Internacionalni naučno-stručni skup Građevinarstvo - nauka i praksa, Žabljak, 7-11. 03. 2016.. 2016;:41-48.
https://hdl.handle.net/21.15107/rcub_grafar_1500 .
Ćetković, Marina, "Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates" in Zbornik radova / Šesti Internacionalni naučno-stručni skup Građevinarstvo - nauka i praksa, Žabljak, 7-11. 03. 2016. (2016):41-48,
https://hdl.handle.net/21.15107/rcub_grafar_1500 .

Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates

Ćetković, Marina

(University of Montenegro / Faculty of Civil Engineering, 2016)

TY  - CONF
AU  - Ćetković, Marina
PY  - 2016
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1885
AB  - In this paper thermal stability of laminated composite plates is analyzed using layerwise finite element. The weak form of the plate mathematical model is derived using layerwise displacement field of Reddy [1], nonlinear strain-displacement relations (in von Karman sense) and linear orthotropic thermo-mechanical material properties. The weak form is discretized using isoparametric finite element formulation. The nine-node Lagrangian isoparametric element is used to derive element stiffness and geometric stiffness matrix. The originally coded MATLAB program is used to analyze the effects of different boundary conditions on thermo-elastic stability of laminate composite plate. The accuracy of the numerical model is verified by comparison with the available results from the literature.
PB  - University of Montenegro / Faculty of Civil Engineering
PB  - Univerzitet Crne Gore / Građevinski fakultet
C3  - Proceedings / The 6th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2016.
T1  - Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates
T1  - Slojeviti konačni element za analizu termičke stabilnosti laminatnih kompozitnim ploča
EP  - 48
SP  - 41
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1885
ER  - 
@conference{
author = "Ćetković, Marina",
year = "2016",
abstract = "In this paper thermal stability of laminated composite plates is analyzed using layerwise finite element. The weak form of the plate mathematical model is derived using layerwise displacement field of Reddy [1], nonlinear strain-displacement relations (in von Karman sense) and linear orthotropic thermo-mechanical material properties. The weak form is discretized using isoparametric finite element formulation. The nine-node Lagrangian isoparametric element is used to derive element stiffness and geometric stiffness matrix. The originally coded MATLAB program is used to analyze the effects of different boundary conditions on thermo-elastic stability of laminate composite plate. The accuracy of the numerical model is verified by comparison with the available results from the literature.",
publisher = "University of Montenegro / Faculty of Civil Engineering, Univerzitet Crne Gore / Građevinski fakultet",
journal = "Proceedings / The 6th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2016.",
title = "Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates, Slojeviti konačni element za analizu termičke stabilnosti laminatnih kompozitnim ploča",
pages = "48-41",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1885"
}
Ćetković, M.. (2016). Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates. in Proceedings / The 6th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2016.
University of Montenegro / Faculty of Civil Engineering., 41-48.
https://hdl.handle.net/21.15107/rcub_grafar_1885
Ćetković M. Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates. in Proceedings / The 6th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2016.. 2016;:41-48.
https://hdl.handle.net/21.15107/rcub_grafar_1885 .
Ćetković, Marina, "Layerwise Finite Element for Thermal Stability Analysis of Laminated Composite Plates" in Proceedings / The 6th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2016. (2016):41-48,
https://hdl.handle.net/21.15107/rcub_grafar_1885 .

Nelinearna termo-mehanicka analiza laminatnih kompozitnih ploca primenom slojevitih konačnih elemenata

Ćetković, Marina

(Beograd: Univerzitet u Beogradu, Građevinski fakultet ; Podgorica: Univerzitet Crne Gore, Građevinski fakultet, 2016)

TY  - CHAP
AU  - Ćetković, Marina
PY  - 2016
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1071
PB  - Beograd: Univerzitet u Beogradu, Građevinski fakultet ; Podgorica: Univerzitet Crne Gore, Građevinski fakultet
T2  - Savremeni problemi teorije konstrukcija : monografija posvećena uspomeni na profesora Đorđa Vuksanov
T1  - Nelinearna termo-mehanicka analiza laminatnih kompozitnih ploca primenom slojevitih konačnih elemenata
EP  - 24
SP  - 11
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1071
ER  - 
@inbook{
author = "Ćetković, Marina",
year = "2016",
publisher = "Beograd: Univerzitet u Beogradu, Građevinski fakultet ; Podgorica: Univerzitet Crne Gore, Građevinski fakultet",
journal = "Savremeni problemi teorije konstrukcija : monografija posvećena uspomeni na profesora Đorđa Vuksanov",
booktitle = "Nelinearna termo-mehanicka analiza laminatnih kompozitnih ploca primenom slojevitih konačnih elemenata",
pages = "24-11",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1071"
}
Ćetković, M.. (2016). Nelinearna termo-mehanicka analiza laminatnih kompozitnih ploca primenom slojevitih konačnih elemenata. in Savremeni problemi teorije konstrukcija : monografija posvećena uspomeni na profesora Đorđa Vuksanov
Beograd: Univerzitet u Beogradu, Građevinski fakultet ; Podgorica: Univerzitet Crne Gore, Građevinski fakultet., 11-24.
https://hdl.handle.net/21.15107/rcub_grafar_1071
Ćetković M. Nelinearna termo-mehanicka analiza laminatnih kompozitnih ploca primenom slojevitih konačnih elemenata. in Savremeni problemi teorije konstrukcija : monografija posvećena uspomeni na profesora Đorđa Vuksanov. 2016;:11-24.
https://hdl.handle.net/21.15107/rcub_grafar_1071 .
Ćetković, Marina, "Nelinearna termo-mehanicka analiza laminatnih kompozitnih ploca primenom slojevitih konačnih elemenata" in Savremeni problemi teorije konstrukcija : monografija posvećena uspomeni na profesora Đorđa Vuksanov (2016):11-24,
https://hdl.handle.net/21.15107/rcub_grafar_1071 .

Thermal buckling of laminated composite plates using layerwise displacement model

Ćetković, Marina

(Elsevier Ltd, 2016)

TY  - JOUR
AU  - Ćetković, Marina
PY  - 2016
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/797
AB  - In this paper thermal buckling of laminated composite plates, based on Layerwise Theory of Reddy and new version of Layerwise Theory of Reddy, presented for the first time, are formulated using the principle of virtual displacements (PVD). The Navier's analytical solution is derived from the strong form, while the weak form is discretized using the isoparametric finite element approximation. The nine-node Lagrangian isoparametric element is used to derive element stiffness and geometric stiffness matrix. The originally coded MATI.AB program is used to investigate the effects of temperature distribution, side to thickness ratio, aspect ratio, modulus ratio E-1/E-2, thermal expansion coefficient ratio alpha(2)/alpha(1), mesh refinement and boundary conditions on thermal buckling of isotropic, orthotropic and laminated composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature and some new results are presented.
PB  - Elsevier Ltd
T2  - Composite Structures
T1  - Thermal buckling of laminated composite plates using layerwise displacement model
EP  - 253
SP  - 238
VL  - 142
DO  - 10.1016/j.compstruct.2016.01.082
ER  - 
@article{
author = "Ćetković, Marina",
year = "2016",
abstract = "In this paper thermal buckling of laminated composite plates, based on Layerwise Theory of Reddy and new version of Layerwise Theory of Reddy, presented for the first time, are formulated using the principle of virtual displacements (PVD). The Navier's analytical solution is derived from the strong form, while the weak form is discretized using the isoparametric finite element approximation. The nine-node Lagrangian isoparametric element is used to derive element stiffness and geometric stiffness matrix. The originally coded MATI.AB program is used to investigate the effects of temperature distribution, side to thickness ratio, aspect ratio, modulus ratio E-1/E-2, thermal expansion coefficient ratio alpha(2)/alpha(1), mesh refinement and boundary conditions on thermal buckling of isotropic, orthotropic and laminated composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature and some new results are presented.",
publisher = "Elsevier Ltd",
journal = "Composite Structures",
title = "Thermal buckling of laminated composite plates using layerwise displacement model",
pages = "253-238",
volume = "142",
doi = "10.1016/j.compstruct.2016.01.082"
}
Ćetković, M.. (2016). Thermal buckling of laminated composite plates using layerwise displacement model. in Composite Structures
Elsevier Ltd., 142, 238-253.
https://doi.org/10.1016/j.compstruct.2016.01.082
Ćetković M. Thermal buckling of laminated composite plates using layerwise displacement model. in Composite Structures. 2016;142:238-253.
doi:10.1016/j.compstruct.2016.01.082 .
Ćetković, Marina, "Thermal buckling of laminated composite plates using layerwise displacement model" in Composite Structures, 142 (2016):238-253,
https://doi.org/10.1016/j.compstruct.2016.01.082 . .
51
34
57

Thermo-elastic stability of angle-ply laminates - application of layerwise finite elements

Ćetković, Marina; Gyorgy, Lenart

(Institut za ispitivanje materijala, Beograd, 2016)

TY  - JOUR
AU  - Ćetković, Marina
AU  - Gyorgy, Lenart
PY  - 2016
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/752
AB  - In this paper thermal buckling analysis of angle-ply laminates is analysed using Generalized Layerwise Plate Theory (GLPT) of Reddy, /1/. The finite element solution is derived from the weak form of the problem. The nine-node Lagrangian isoparametric finite element is used to derive the element stiffness matrix and geometric stiffness matrix. The originally coded MATLAB programme is used to analyse the effects of side to thickness ratio a/b, aspect ratio a/b, ply-orientation angle theta, modulus ratio E-1/E-2, thermal expansion coefficient ratio. alpha(2)/alpha(1,) temperature distribution and different boundary conditions, on thermoelastic stability of laminated composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature.
PB  - Institut za ispitivanje materijala, Beograd
T2  - Structural Integrity and Life-Integritet I Vek Konstrukcija
T1  - Thermo-elastic stability of angle-ply laminates - application of layerwise finite elements
EP  - 48
IS  - 1
SP  - 43
VL  - 16
UR  - https://hdl.handle.net/21.15107/rcub_grafar_752
ER  - 
@article{
author = "Ćetković, Marina and Gyorgy, Lenart",
year = "2016",
abstract = "In this paper thermal buckling analysis of angle-ply laminates is analysed using Generalized Layerwise Plate Theory (GLPT) of Reddy, /1/. The finite element solution is derived from the weak form of the problem. The nine-node Lagrangian isoparametric finite element is used to derive the element stiffness matrix and geometric stiffness matrix. The originally coded MATLAB programme is used to analyse the effects of side to thickness ratio a/b, aspect ratio a/b, ply-orientation angle theta, modulus ratio E-1/E-2, thermal expansion coefficient ratio. alpha(2)/alpha(1,) temperature distribution and different boundary conditions, on thermoelastic stability of laminated composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature.",
publisher = "Institut za ispitivanje materijala, Beograd",
journal = "Structural Integrity and Life-Integritet I Vek Konstrukcija",
title = "Thermo-elastic stability of angle-ply laminates - application of layerwise finite elements",
pages = "48-43",
number = "1",
volume = "16",
url = "https://hdl.handle.net/21.15107/rcub_grafar_752"
}
Ćetković, M.,& Gyorgy, L.. (2016). Thermo-elastic stability of angle-ply laminates - application of layerwise finite elements. in Structural Integrity and Life-Integritet I Vek Konstrukcija
Institut za ispitivanje materijala, Beograd., 16(1), 43-48.
https://hdl.handle.net/21.15107/rcub_grafar_752
Ćetković M, Gyorgy L. Thermo-elastic stability of angle-ply laminates - application of layerwise finite elements. in Structural Integrity and Life-Integritet I Vek Konstrukcija. 2016;16(1):43-48.
https://hdl.handle.net/21.15107/rcub_grafar_752 .
Ćetković, Marina, Gyorgy, Lenart, "Thermo-elastic stability of angle-ply laminates - application of layerwise finite elements" in Structural Integrity and Life-Integritet I Vek Konstrukcija, 16, no. 1 (2016):43-48,
https://hdl.handle.net/21.15107/rcub_grafar_752 .
3
7

Практикум из Статике конструкција

Vuksanović, Đorđe; Ćetković, Marina

(Академска мисао, Београд, 2015, 2015)

TY  - GEN
AU  - Vuksanović, Đorđe
AU  - Ćetković, Marina
PY  - 2015
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1898
AB  - У књизи је 	приказана материја која се у оквиру вежбања из предмета  Статика конструкација излаже студентима треће године основних академских студија Грађевинарство ─ модул К на Грађевинском факултету Универзитета у Београду. Овај практикум смо припремили са жељом да олакшамо студентима праћење наставе и омогућимо им успешно савлађивање градива као и ефикасну припрему испита. Да би практикум успешно одгворио својој намени претпоставља се да су студенти у довољној мери упознати са теоријским основама предмета тако да могу разумети методе и поступке примењене при решавању приказаних задатака. Без обзира на ову чињеницу у оквиру појединих поглавља изложена је у најмањем могућем обиму теорија потребна за разумевање и успешно решавање проблема који следе. Сматрамо да ће постојање једног овако замишљеног практикума омогућити студентима да се активније укључе у процес вежби из предмета Статика конструкција. При изради књиге учињен је знатан напор да се елиминишу могуће грешке, међутим свесни смо чињенице да су оне увек  могуће, па смо унапред захвални свим добронамерним примедбама и сугестијама.
PB  - Академска мисао, Београд, 2015
T2  - Академска мисао, Београд, 2015
T1  - Практикум из Статике конструкција
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1898
ER  - 
@misc{
author = "Vuksanović, Đorđe and Ćetković, Marina",
year = "2015",
abstract = "У књизи је 	приказана материја која се у оквиру вежбања из предмета  Статика конструкација излаже студентима треће године основних академских студија Грађевинарство ─ модул К на Грађевинском факултету Универзитета у Београду. Овај практикум смо припремили са жељом да олакшамо студентима праћење наставе и омогућимо им успешно савлађивање градива као и ефикасну припрему испита. Да би практикум успешно одгворио својој намени претпоставља се да су студенти у довољној мери упознати са теоријским основама предмета тако да могу разумети методе и поступке примењене при решавању приказаних задатака. Без обзира на ову чињеницу у оквиру појединих поглавља изложена је у најмањем могућем обиму теорија потребна за разумевање и успешно решавање проблема који следе. Сматрамо да ће постојање једног овако замишљеног практикума омогућити студентима да се активније укључе у процес вежби из предмета Статика конструкција. При изради књиге учињен је знатан напор да се елиминишу могуће грешке, међутим свесни смо чињенице да су оне увек  могуће, па смо унапред захвални свим добронамерним примедбама и сугестијама.",
publisher = "Академска мисао, Београд, 2015",
journal = "Академска мисао, Београд, 2015",
title = "Практикум из Статике конструкција",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1898"
}
Vuksanović, Đ.,& Ćetković, M.. (2015). Практикум из Статике конструкција. in Академска мисао, Београд, 2015
Академска мисао, Београд, 2015..
https://hdl.handle.net/21.15107/rcub_grafar_1898
Vuksanović Đ, Ćetković M. Практикум из Статике конструкција. in Академска мисао, Београд, 2015. 2015;.
https://hdl.handle.net/21.15107/rcub_grafar_1898 .
Vuksanović, Đorđe, Ćetković, Marina, "Практикум из Статике конструкција" in Академска мисао, Београд, 2015 (2015),
https://hdl.handle.net/21.15107/rcub_grafar_1898 .

Thermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement model

Ćetković, Marina

(Elsevier Ltd, 2015)

TY  - JOUR
AU  - Ćetković, Marina
PY  - 2015
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/729
AB  - The objective of this paper is thermo-mechanical bending of laminated composite and sandwich plates subjected to mechanical load and linearly varying through the thickness temperature field. Mathematical model, based on layer-wise displacement field of Reddy, is formulated using small deflection linear-elasticity theory. The principle of virtual displacements (PVD) is used to obtain the strong and the weak form of the mathematical model. The weak form is discretized using the isoparametric finite element approximation, while the analytical solution is derived from the strong form. The originally coded MATLAB program is used to investigate the influence of plate geometry and degree of material orthotropy on thermo-mechanical response of laminate composite and sandwich plates. The accuracy of the numerical model is verified by comparison with the available results from the literature and some new results are presented.
PB  - Elsevier Ltd
T2  - Composite Structures
T1  - Thermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement model
EP  - 399
SP  - 388
VL  - 125
DO  - 10.1016/j.compstruct.2015.01.051
ER  - 
@article{
author = "Ćetković, Marina",
year = "2015",
abstract = "The objective of this paper is thermo-mechanical bending of laminated composite and sandwich plates subjected to mechanical load and linearly varying through the thickness temperature field. Mathematical model, based on layer-wise displacement field of Reddy, is formulated using small deflection linear-elasticity theory. The principle of virtual displacements (PVD) is used to obtain the strong and the weak form of the mathematical model. The weak form is discretized using the isoparametric finite element approximation, while the analytical solution is derived from the strong form. The originally coded MATLAB program is used to investigate the influence of plate geometry and degree of material orthotropy on thermo-mechanical response of laminate composite and sandwich plates. The accuracy of the numerical model is verified by comparison with the available results from the literature and some new results are presented.",
publisher = "Elsevier Ltd",
journal = "Composite Structures",
title = "Thermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement model",
pages = "399-388",
volume = "125",
doi = "10.1016/j.compstruct.2015.01.051"
}
Ćetković, M.. (2015). Thermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement model. in Composite Structures
Elsevier Ltd., 125, 388-399.
https://doi.org/10.1016/j.compstruct.2015.01.051
Ćetković M. Thermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement model. in Composite Structures. 2015;125:388-399.
doi:10.1016/j.compstruct.2015.01.051 .
Ćetković, Marina, "Thermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement model" in Composite Structures, 125 (2015):388-399,
https://doi.org/10.1016/j.compstruct.2015.01.051 . .
40
28
48

Thermal Analysis of Laminated Composite and Sandwich Plates Using Layerwise Finite Element

Ćetković, Marina; Vuksanović, Đorđe

(2014)

TY  - JOUR
AU  - Ćetković, Marina
AU  - Vuksanović, Đorđe
PY  - 2014
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1017
AB  - In this paper the quasi static response of laminated composite and sandwich plates subjected to lineary
varaying through the thickness and sinusoidall distributed in plane temperature field, is analyzed. Mathematical
model, based on layer-wise displacement field of Reddy [15], is formulated using small deflection linear-elasticity
theory. The principle of virtual displacements (PVD) is used to obtain the weak form of the mathematical model.
The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB
program is used to investigate the influence of plate thickness on thermo-elastic response of laminate composite
and sandwich plates.
T2  - Construction of Unique Buildings and Structures
T1  - Thermal Analysis of Laminated Composite and Sandwich Plates Using Layerwise Finite Element
EP  - 14
IS  - 20
SP  - 7
VL  - 5
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1017
ER  - 
@article{
author = "Ćetković, Marina and Vuksanović, Đorđe",
year = "2014",
abstract = "In this paper the quasi static response of laminated composite and sandwich plates subjected to lineary
varaying through the thickness and sinusoidall distributed in plane temperature field, is analyzed. Mathematical
model, based on layer-wise displacement field of Reddy [15], is formulated using small deflection linear-elasticity
theory. The principle of virtual displacements (PVD) is used to obtain the weak form of the mathematical model.
The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB
program is used to investigate the influence of plate thickness on thermo-elastic response of laminate composite
and sandwich plates.",
journal = "Construction of Unique Buildings and Structures",
title = "Thermal Analysis of Laminated Composite and Sandwich Plates Using Layerwise Finite Element",
pages = "14-7",
number = "20",
volume = "5",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1017"
}
Ćetković, M.,& Vuksanović, Đ.. (2014). Thermal Analysis of Laminated Composite and Sandwich Plates Using Layerwise Finite Element. in Construction of Unique Buildings and Structures, 5(20), 7-14.
https://hdl.handle.net/21.15107/rcub_grafar_1017
Ćetković M, Vuksanović Đ. Thermal Analysis of Laminated Composite and Sandwich Plates Using Layerwise Finite Element. in Construction of Unique Buildings and Structures. 2014;5(20):7-14.
https://hdl.handle.net/21.15107/rcub_grafar_1017 .
Ćetković, Marina, Vuksanović, Đorđe, "Thermal Analysis of Laminated Composite and Sandwich Plates Using Layerwise Finite Element" in Construction of Unique Buildings and Structures, 5, no. 20 (2014):7-14,
https://hdl.handle.net/21.15107/rcub_grafar_1017 .

Thermal Analysis of Laminated Composite and Sandwich Plate Using Layerwise Finite Element

Ćetković, Marina; Vuksanović, Đorđe

(University of Montenegro, Faculty of Civil Engineering, 2014)

TY  - CONF
AU  - Ćetković, Marina
AU  - Vuksanović, Đorđe
PY  - 2014
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1884
AB  - In this paper the quasi static response of laminated composite and sandwich plates subjected to lineary varaying through the thickness and sinusoidall distributed in plane temperature field, is analyzed. Mathematical model, based on layer-wise displacement field of Reddy [15], is formulated using small deflection linear-elasticity theory. The principle of virtual displacements (PVD) is used to obtain the weak form of the mathematical model. The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB program is used to investigate the influence of plate thickness on thermo-elastic response of laminate composite and sandwich plates. The accuracy of the numerical model is verified by comparison with the available results from the literature.
AB  - U ovom radu analiziran je kvazi statički odgovor laminatnih kompozitnih i sendvič ploča ploča izloženih temperaturnom polju linearno promenlivom po debljini i sinusoiudalno promenlijvom u ravni. Matematički model, zasnovan na slojevitom polju pomeranja koje je predložio Reddy [15], formulisan je koristeći pretpostavke o geometrijskoj, materijalnoj i statičkoj linearnosti problema. Princip virtulanih pomeranja je primenjen za dobijanje slabe forme matematičkog modela. Slaba forma je diskretizovana koristeći izoparametarsku aproksimaciju konačnim elementom. Originalan MATLAB računski program je korišćen za analizu uticaja razlicitih debljina ploče na termo-elastičan odgovor laminatnih kompozitnih i sendvič ploča. Tačnost numeričkog modela je potvrđena poređenjem sa rešenjima iz literature.
PB  - University of Montenegro, Faculty of Civil Engineering
PB  - Univerzitet Crne Gore, Građevinski fakultet
C3  - Proceedings / The 5th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2014.
T1  - Thermal Analysis of Laminated Composite and Sandwich Plate Using Layerwise Finite Element
T1  - Termička analiza laminatnih kompozitnih i sendvič ploča primenom slojevitog konačnog elementa
EP  - 52
SP  - 45
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1884
ER  - 
@conference{
author = "Ćetković, Marina and Vuksanović, Đorđe",
year = "2014",
abstract = "In this paper the quasi static response of laminated composite and sandwich plates subjected to lineary varaying through the thickness and sinusoidall distributed in plane temperature field, is analyzed. Mathematical model, based on layer-wise displacement field of Reddy [15], is formulated using small deflection linear-elasticity theory. The principle of virtual displacements (PVD) is used to obtain the weak form of the mathematical model. The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB program is used to investigate the influence of plate thickness on thermo-elastic response of laminate composite and sandwich plates. The accuracy of the numerical model is verified by comparison with the available results from the literature., U ovom radu analiziran je kvazi statički odgovor laminatnih kompozitnih i sendvič ploča ploča izloženih temperaturnom polju linearno promenlivom po debljini i sinusoiudalno promenlijvom u ravni. Matematički model, zasnovan na slojevitom polju pomeranja koje je predložio Reddy [15], formulisan je koristeći pretpostavke o geometrijskoj, materijalnoj i statičkoj linearnosti problema. Princip virtulanih pomeranja je primenjen za dobijanje slabe forme matematičkog modela. Slaba forma je diskretizovana koristeći izoparametarsku aproksimaciju konačnim elementom. Originalan MATLAB računski program je korišćen za analizu uticaja razlicitih debljina ploče na termo-elastičan odgovor laminatnih kompozitnih i sendvič ploča. Tačnost numeričkog modela je potvrđena poređenjem sa rešenjima iz literature.",
publisher = "University of Montenegro, Faculty of Civil Engineering, Univerzitet Crne Gore, Građevinski fakultet",
journal = "Proceedings / The 5th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2014.",
title = "Thermal Analysis of Laminated Composite and Sandwich Plate Using Layerwise Finite Element, Termička analiza laminatnih kompozitnih i sendvič ploča primenom slojevitog konačnog elementa",
pages = "52-45",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1884"
}
Ćetković, M.,& Vuksanović, Đ.. (2014). Thermal Analysis of Laminated Composite and Sandwich Plate Using Layerwise Finite Element. in Proceedings / The 5th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2014.
University of Montenegro, Faculty of Civil Engineering., 45-52.
https://hdl.handle.net/21.15107/rcub_grafar_1884
Ćetković M, Vuksanović Đ. Thermal Analysis of Laminated Composite and Sandwich Plate Using Layerwise Finite Element. in Proceedings / The 5th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2014.. 2014;:45-52.
https://hdl.handle.net/21.15107/rcub_grafar_1884 .
Ćetković, Marina, Vuksanović, Đorđe, "Thermal Analysis of Laminated Composite and Sandwich Plate Using Layerwise Finite Element" in Proceedings / The 5th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2014. (2014):45-52,
https://hdl.handle.net/21.15107/rcub_grafar_1884 .

Free vibrations of laminated composite plates using layerwise displacement model

Ćetković, Marina; Vuksanović, Đorđe

(Transilvania University Publishing House Brasov, Romania, 2012)

TY  - CONF
AU  - Ćetković, Marina
AU  - Vuksanović, Đorđe
PY  - 2012
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1880
AB  - In this paper Generalized Layer Wise Plate Theory of Reddy (GLPT) is used to formulate an isoparametric finite element model for free vibration of laminated composite plates. With the assumed displacement field, linear strain displacement relations and linear elastic orthotropic material properties for each lamina, virtual work statement is utilized in order to formulate isoparametric finite element model. The original MATLAB computer program is coded for finite element solution. Some new results using GLPT finite element model for soft core sandwich plate is presented, which may be used as the guideline for their optimal design in the laboratory.
PB  - Transilvania University Publishing House Brasov, Romania
C3  - Book of Abstracts / 11th Youth Symposium on Experimental Solid Mechanics, Brasov, Romania, 2012
T1  - Free vibrations of laminated composite plates using layerwise displacement model
EP  - 131
SP  - 130
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1880
ER  - 
@conference{
author = "Ćetković, Marina and Vuksanović, Đorđe",
year = "2012",
abstract = "In this paper Generalized Layer Wise Plate Theory of Reddy (GLPT) is used to formulate an isoparametric finite element model for free vibration of laminated composite plates. With the assumed displacement field, linear strain displacement relations and linear elastic orthotropic material properties for each lamina, virtual work statement is utilized in order to formulate isoparametric finite element model. The original MATLAB computer program is coded for finite element solution. Some new results using GLPT finite element model for soft core sandwich plate is presented, which may be used as the guideline for their optimal design in the laboratory.",
publisher = "Transilvania University Publishing House Brasov, Romania",
journal = "Book of Abstracts / 11th Youth Symposium on Experimental Solid Mechanics, Brasov, Romania, 2012",
title = "Free vibrations of laminated composite plates using layerwise displacement model",
pages = "131-130",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1880"
}
Ćetković, M.,& Vuksanović, Đ.. (2012). Free vibrations of laminated composite plates using layerwise displacement model. in Book of Abstracts / 11th Youth Symposium on Experimental Solid Mechanics, Brasov, Romania, 2012
Transilvania University Publishing House Brasov, Romania., 130-131.
https://hdl.handle.net/21.15107/rcub_grafar_1880
Ćetković M, Vuksanović Đ. Free vibrations of laminated composite plates using layerwise displacement model. in Book of Abstracts / 11th Youth Symposium on Experimental Solid Mechanics, Brasov, Romania, 2012. 2012;:130-131.
https://hdl.handle.net/21.15107/rcub_grafar_1880 .
Ćetković, Marina, Vuksanović, Đorđe, "Free vibrations of laminated composite plates using layerwise displacement model" in Book of Abstracts / 11th Youth Symposium on Experimental Solid Mechanics, Brasov, Romania, 2012 (2012):130-131,
https://hdl.handle.net/21.15107/rcub_grafar_1880 .

Influence of Boundary Conditions on Nonlinear Response of Laminated Composite Plates

Ćetković, Marina; Vuksanović, Đorđe

(University of Montenegro, Faculty of Civil Engineering, 2012)

TY  - CONF
AU  - Ćetković, Marina
AU  - Vuksanović, Đorđe
PY  - 2012
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/1883
AB  - In this paper the influence of different boundary conditions on geometrically nonlinear response of laminated composite plates is analyzed. Mathematical model, based on layer-wise displacement field of Reddy [1], is formulated using the von Karman, small strain large deflection theory. The principle if virtual displacements (PVD) is used to obtain the weak form of the problem. The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB program is used to investigate the influence of different boundary conditions on geometrically nonlinear response of laminate composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature.
AB  - U ovom radu analiziran je uticaj različitih graničnih uslova na geometrijski nelinearan odgovor laminatnih kompozitnih ploča. Matematički model, zasnovan na slojevitom polju pomeranja koje je predložio Reddy [1], formulisan je koristeći von Karman’ovu teoriju velikih pomeranja i malih deformacija. Princip virtulanih pomeranja je primenjen za dobijanje slabe forme problema. Slaba forma je diskretizovana koristeći izoparametarsku aproksimaciju konačnim elementom. Originalan MATLAB računski program je korišćen za analizu uticaja razlicitih graničnih uslova na nelinearna odgovor laminatnih kompozitnih ploča. Tačnost numeričkog modela je potvrđena poređenjem sa rešenjima iz literature.
PB  - University of Montenegro, Faculty of Civil Engineering
C3  - Proceedings / The 4th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2012.
T1  - Influence of Boundary Conditions on Nonlinear Response of Laminated Composite Plates
T1  - Uticaj graničnih uslova na nelinearan odgovor laminatnih kompozitnih ploča
EP  - 58
SP  - 51
UR  - https://hdl.handle.net/21.15107/rcub_grafar_1883
ER  - 
@conference{
author = "Ćetković, Marina and Vuksanović, Đorđe",
year = "2012",
abstract = "In this paper the influence of different boundary conditions on geometrically nonlinear response of laminated composite plates is analyzed. Mathematical model, based on layer-wise displacement field of Reddy [1], is formulated using the von Karman, small strain large deflection theory. The principle if virtual displacements (PVD) is used to obtain the weak form of the problem. The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB program is used to investigate the influence of different boundary conditions on geometrically nonlinear response of laminate composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature., U ovom radu analiziran je uticaj različitih graničnih uslova na geometrijski nelinearan odgovor laminatnih kompozitnih ploča. Matematički model, zasnovan na slojevitom polju pomeranja koje je predložio Reddy [1], formulisan je koristeći von Karman’ovu teoriju velikih pomeranja i malih deformacija. Princip virtulanih pomeranja je primenjen za dobijanje slabe forme problema. Slaba forma je diskretizovana koristeći izoparametarsku aproksimaciju konačnim elementom. Originalan MATLAB računski program je korišćen za analizu uticaja razlicitih graničnih uslova na nelinearna odgovor laminatnih kompozitnih ploča. Tačnost numeričkog modela je potvrđena poređenjem sa rešenjima iz literature.",
publisher = "University of Montenegro, Faculty of Civil Engineering",
journal = "Proceedings / The 4th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2012.",
title = "Influence of Boundary Conditions on Nonlinear Response of Laminated Composite Plates, Uticaj graničnih uslova na nelinearan odgovor laminatnih kompozitnih ploča",
pages = "58-51",
url = "https://hdl.handle.net/21.15107/rcub_grafar_1883"
}
Ćetković, M.,& Vuksanović, Đ.. (2012). Influence of Boundary Conditions on Nonlinear Response of Laminated Composite Plates. in Proceedings / The 4th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2012.
University of Montenegro, Faculty of Civil Engineering., 51-58.
https://hdl.handle.net/21.15107/rcub_grafar_1883
Ćetković M, Vuksanović Đ. Influence of Boundary Conditions on Nonlinear Response of Laminated Composite Plates. in Proceedings / The 4th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2012.. 2012;:51-58.
https://hdl.handle.net/21.15107/rcub_grafar_1883 .
Ćetković, Marina, Vuksanović, Đorđe, "Influence of Boundary Conditions on Nonlinear Response of Laminated Composite Plates" in Proceedings / The 4th International Conference Civil Engineering - Science & Practice, Žabljak, Montenegro, 2012. (2012):51-58,
https://hdl.handle.net/21.15107/rcub_grafar_1883 .

Influence of boundary conditions on nonlinear response of laminated composite plates

Ćetković, Marina; Vuksanović, Đorđe; Knežević, Miloš; Samardzioska, Todorka; Cvetkovska, Meri

(Institut za istraživanja i projektovanja u privredi, Beograd, 2012)

TY  - JOUR
AU  - Ćetković, Marina
AU  - Vuksanović, Đorđe
AU  - Knežević, Miloš
AU  - Samardzioska, Todorka
AU  - Cvetkovska, Meri
PY  - 2012
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/422
AB  - In this paper the influence of different boundary conditions on geometrically nonlinear response of laminated composite plates is analyzed. Mathematical model, based on layer-wise displacement field of Reddy [1], is formulated using the von Karman, small strain large deflection theory. The principle if virtual displacements (PVD) is used to obtain the weak form of the problem. The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB program is used to investigate the influence of different boundary conditions on geometrically nonlinear response of laminate composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature.
AB  - U ovom radu analiziran je uticaj različitih graničnih uslova na geometrijski nelinearan odgovor laminatnih kompozitnih ploča. Matematički model, zasnovan na slojevitom polju pomeranja koje je predložio Reddy [1], formulisan je koristeći von Karman'ovu teoriju velikih pomeranja i malih deformacija. Princip virtulanih pomeranja je primenjen za dobijanje slabe forme problema. Slaba forma je diskretizovana koristeći izoparametarsku aproksimaciju konačnim elementom. Originalan MATLAB računski program je korišćen za analizu uticaja različitih graničnih uslova na nelinearna odgovor laminatnih kompozitnih ploča. Tačnost numeričkog modela je potvrđena poređenjem sa rešenjima iz literature. .
PB  - Institut za istraživanja i projektovanja u privredi, Beograd
T2  - Journal of Applied Engineering Science
T1  - Influence of boundary conditions on nonlinear response of laminated composite plates
T1  - Uticaj graničnih uslova na nelinearan odgovor laminatnih kompozitnih ploča
EP  - 36
IS  - 1
SP  - 31
VL  - 10
DO  - 10.5937/jaes10-1662
ER  - 
@article{
author = "Ćetković, Marina and Vuksanović, Đorđe and Knežević, Miloš and Samardzioska, Todorka and Cvetkovska, Meri",
year = "2012",
abstract = "In this paper the influence of different boundary conditions on geometrically nonlinear response of laminated composite plates is analyzed. Mathematical model, based on layer-wise displacement field of Reddy [1], is formulated using the von Karman, small strain large deflection theory. The principle if virtual displacements (PVD) is used to obtain the weak form of the problem. The weak form is discretized utilizing isoparametric finite element approximation. The originally coded MATLAB program is used to investigate the influence of different boundary conditions on geometrically nonlinear response of laminate composite plates. The accuracy of the numerical model is verified by comparison with the available results from the literature., U ovom radu analiziran je uticaj različitih graničnih uslova na geometrijski nelinearan odgovor laminatnih kompozitnih ploča. Matematički model, zasnovan na slojevitom polju pomeranja koje je predložio Reddy [1], formulisan je koristeći von Karman'ovu teoriju velikih pomeranja i malih deformacija. Princip virtulanih pomeranja je primenjen za dobijanje slabe forme problema. Slaba forma je diskretizovana koristeći izoparametarsku aproksimaciju konačnim elementom. Originalan MATLAB računski program je korišćen za analizu uticaja različitih graničnih uslova na nelinearna odgovor laminatnih kompozitnih ploča. Tačnost numeričkog modela je potvrđena poređenjem sa rešenjima iz literature. .",
publisher = "Institut za istraživanja i projektovanja u privredi, Beograd",
journal = "Journal of Applied Engineering Science",
title = "Influence of boundary conditions on nonlinear response of laminated composite plates, Uticaj graničnih uslova na nelinearan odgovor laminatnih kompozitnih ploča",
pages = "36-31",
number = "1",
volume = "10",
doi = "10.5937/jaes10-1662"
}
Ćetković, M., Vuksanović, Đ., Knežević, M., Samardzioska, T.,& Cvetkovska, M.. (2012). Influence of boundary conditions on nonlinear response of laminated composite plates. in Journal of Applied Engineering Science
Institut za istraživanja i projektovanja u privredi, Beograd., 10(1), 31-36.
https://doi.org/10.5937/jaes10-1662
Ćetković M, Vuksanović Đ, Knežević M, Samardzioska T, Cvetkovska M. Influence of boundary conditions on nonlinear response of laminated composite plates. in Journal of Applied Engineering Science. 2012;10(1):31-36.
doi:10.5937/jaes10-1662 .
Ćetković, Marina, Vuksanović, Đorđe, Knežević, Miloš, Samardzioska, Todorka, Cvetkovska, Meri, "Influence of boundary conditions on nonlinear response of laminated composite plates" in Journal of Applied Engineering Science, 10, no. 1 (2012):31-36,
https://doi.org/10.5937/jaes10-1662 . .
2
1

Vibrations of isotropic, orthotropic and laminated composite plates with various boundary conditions

Ćetković, Marina; Vuksanović, Đorđe

(Univerzitet u Kragujevcu - Fakultet inženjerskih nauka, Kragujevac, 2012)

TY  - JOUR
AU  - Ćetković, Marina
AU  - Vuksanović, Đorđe
PY  - 2012
UR  - https://grafar.grf.bg.ac.rs/handle/123456789/424
AB  - In this paper Generalized Layer Wise Plate Theory of Reddy (GLPT) is used to formulate an isoparametric finite element model for free vibrations of isotropic, orthotropic and laminated composite plates. With the assumed displacement field, linear strain displacement relations and linear elastic orthotropic material properties for each lamina, governing differential equations of motion are derived using Hamilton‘s principle. Virtual work statement is then utilized to formulate isoparametric finite element model. The original MATLAB computer program is coded for finite element solution. The parametric effects of plate aspect ratio b / a , side-tothickness ratio a / h , degree of orthotropy 1 2 E / E and boundary conditions on free vibration response of isotropic, orthotropic and anisotropic plates are analyzed. The accuracy of the present formulation is demonstrated through a number of examples and by comparison with results available from the literature.
AB  - U ovom radu primenom Opšte laminatne teorije ploča (Generalized Layerwise Plate Theory-GLPT), koju je postavio Reddy, formulisan je izoparametarski model konačnog elementa za problem slobodnih vibracija izotropnih, ortotropnih i laminatnih kompozitnih ploča. Osnovne diferencijalne jednačine kretanja izvedene su primenom Hamilton-ovog principa, koristeći pretpostavljeno polje pomeranja, linearne veze deformacija i pomeranja i linearno elastičan ortotropan materijal za svaku od lamina. Princip virtuelnog rada potom je iskorišćen za formulisanje izoparametarskog modela konačnog elementa. Originalni računarski program napisan je za rešenje po Metodi konačnih elemenata, koristeći MATLAB programski jezik. Analiziran je parametarski uticaj odnosa strana ploče , strane prema debljini ploče , stepena ortotropije i graničnih uslova na slobodne vibracije izotropnih, ortotropnih i anizotropnih ploča. Tačnost predstavljene formulacije potvrđena je kroz niz primera i njihovim poređenjem sa rešenjima iz literature.
PB  - Univerzitet u Kragujevcu - Fakultet inženjerskih nauka, Kragujevac
T2  - Journal of Serbian Society for Computational Mechanics
T1  - Vibrations of isotropic, orthotropic and laminated composite plates with various boundary conditions
T1  - Vibracije izotropnih, ortotropnih i laminatnih kompozitnih ploča sa različitim graničnim uslovima oslanjanja
EP  - 96
IS  - 1
SP  - 83
VL  - 6
UR  - https://hdl.handle.net/21.15107/rcub_grafar_424
ER  - 
@article{
author = "Ćetković, Marina and Vuksanović, Đorđe",
year = "2012",
abstract = "In this paper Generalized Layer Wise Plate Theory of Reddy (GLPT) is used to formulate an isoparametric finite element model for free vibrations of isotropic, orthotropic and laminated composite plates. With the assumed displacement field, linear strain displacement relations and linear elastic orthotropic material properties for each lamina, governing differential equations of motion are derived using Hamilton‘s principle. Virtual work statement is then utilized to formulate isoparametric finite element model. The original MATLAB computer program is coded for finite element solution. The parametric effects of plate aspect ratio b / a , side-tothickness ratio a / h , degree of orthotropy 1 2 E / E and boundary conditions on free vibration response of isotropic, orthotropic and anisotropic plates are analyzed. The accuracy of the present formulation is demonstrated through a number of examples and by comparison with results available from the literature., U ovom radu primenom Opšte laminatne teorije ploča (Generalized Layerwise Plate Theory-GLPT), koju je postavio Reddy, formulisan je izoparametarski model konačnog elementa za problem slobodnih vibracija izotropnih, ortotropnih i laminatnih kompozitnih ploča. Osnovne diferencijalne jednačine kretanja izvedene su primenom Hamilton-ovog principa, koristeći pretpostavljeno polje pomeranja, linearne veze deformacija i pomeranja i linearno elastičan ortotropan materijal za svaku od lamina. Princip virtuelnog rada potom je iskorišćen za formulisanje izoparametarskog modela konačnog elementa. Originalni računarski program napisan je za rešenje po Metodi konačnih elemenata, koristeći MATLAB programski jezik. Analiziran je parametarski uticaj odnosa strana ploče , strane prema debljini ploče , stepena ortotropije i graničnih uslova na slobodne vibracije izotropnih, ortotropnih i anizotropnih ploča. Tačnost predstavljene formulacije potvrđena je kroz niz primera i njihovim poređenjem sa rešenjima iz literature.",
publisher = "Univerzitet u Kragujevcu - Fakultet inženjerskih nauka, Kragujevac",
journal = "Journal of Serbian Society for Computational Mechanics",
title = "Vibrations of isotropic, orthotropic and laminated composite plates with various boundary conditions, Vibracije izotropnih, ortotropnih i laminatnih kompozitnih ploča sa različitim graničnim uslovima oslanjanja",
pages = "96-83",
number = "1",
volume = "6",
url = "https://hdl.handle.net/21.15107/rcub_grafar_424"
}
Ćetković, M.,& Vuksanović, Đ.. (2012). Vibrations of isotropic, orthotropic and laminated composite plates with various boundary conditions. in Journal of Serbian Society for Computational Mechanics
Univerzitet u Kragujevcu - Fakultet inženjerskih nauka, Kragujevac., 6(1), 83-96.
https://hdl.handle.net/21.15107/rcub_grafar_424
Ćetković M, Vuksanović Đ. Vibrations of isotropic, orthotropic and laminated composite plates with various boundary conditions. in Journal of Serbian Society for Computational Mechanics. 2012;6(1):83-96.
https://hdl.handle.net/21.15107/rcub_grafar_424 .
Ćetković, Marina, Vuksanović, Đorđe, "Vibrations of isotropic, orthotropic and laminated composite plates with various boundary conditions" in Journal of Serbian Society for Computational Mechanics, 6, no. 1 (2012):83-96,
https://hdl.handle.net/21.15107/rcub_grafar_424 .
4