Buckling analysis of laminated composite plates with an elliptical/circular cutout using FEM

Komur, M. Aydin; Şen, Faruk; Ataş, Akın; Arslan, Nurettin

doi:10.1016/j.advengsoft.2009.09.005

Cited by 94 publications

(30 citation statements)

References 12 publications

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“…of element in plate decreases & increases respectively. In the first part, the result is validated with Komur et.al [9] as shown in Table.3. In this table result were validated The effect of different cut-out shape on buckling load for different stacking sequence is shown in Fig.…”

Section: B Materials Properties and Geometric Modelsupporting

confidence: 67%

“…The mechanical properties of the woven-glass-polyester composite material are listed in Table 1 [9]. In real composite applications, different plate and cutout form may be used owing to design necessities.…”

Section: B Materials Properties and Geometric Modelmentioning

confidence: 99%

“…It has been seen that the numerical buckling analysis are very close to the experimental results. Komur et al [9] analyzed buckling behavior of woven-glass-polyester laminated composite plate having an elliptical/circular cut-out using FEM. Parametric study is also carried out in this paper on various plates based on the shape and position of the elliptical hole.…”

mentioning

confidence: 99%

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Effect of Various Cut-Out on Buckling Analysis of Laminated Composite Plate Using Fe Simulation

2015

International Conference on Advancements and Recent Innovations in Mechanical, Production and Industrial Engineering

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Section: B Materials Properties and Geometric Modelsupporting

confidence: 67%

Section: B Materials Properties and Geometric Modelmentioning

confidence: 99%

mentioning

confidence: 99%

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Effect of Various Cut-Out on Buckling Analysis of Laminated Composite Plate Using Fe Simulation

2015

International Conference on Advancements and Recent Innovations in Mechanical, Production and Industrial Engineering

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“…Many studies have been carried out about the stability of the laminated square plates under cutout shape and size, boundary and loading conditions and orientation of the cut outs in cross ply and angle ply laminates. [1][2].…”

Section: Introductionmentioning

confidence: 99%

Linear Buckling behaviour of Composite Laminate [(θ/-θ)] with various shaped cutout using FEM

et al. 2019

IJEAT

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In this paper, the buckling behavior has been investigated on square laminate made of Woven-glass-polyester composite with various shaped cutouts (i.e., circle, square, vertical rectangle, horizontal rectangle, vertical ellipse, horizontal ellipse) numerically. The composite laminates have been arranged in asymmetrical order as [(θ/-θ)]. The laminated plate that is subjected to uniaxial compression has been emphasized on the laminate along with the effect of layer orientation, effect of cutout ratio and effect of cutout angle. The result shows that the minimum buckling load is obtained at 45° and the maximum buckling load attained at 0° and 90°for all laminates by increasing the layer orientation. For cutout ratio, the maximum and minimum load is obtained for the smallest and largest cutout ratio in all cutout shapes. Increasing the cutout angle, the square cutout exhibits the minimum load at 60°. In elliptical cutouts, the load is decreasing and increasing gradually while they are aligned in along and perpendicular to the loading directions. The rectangular cutouts positioned vertically and horizontally the load is decreasing up to 30° and 60°and then increasing up to 90°.

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“…The effect of cutouts on the buckling behaviour of laminated composites were studied in [16,20]. And more recently, Komur et al, [9] and Ghannadpour et al, [7] studied the buckling behaviour of laminated composites with circular and elliptical cutouts using the finite element method and first order shear deformation theory. Their study was restricted to a limited number of configurations, because the mesh has to conform to the geometry.…”

Section: Introductionmentioning

confidence: 99%

Hygrothermal effects on the free vibration and buckling of laminated composites with cutouts

Natarajan

Deogekar

Ganapathi

et al. 2014

Composite Structures

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Abstract. The effect of moisture concentration and the thermal gradient on the free flexural vibration and buckling of laminated composite plates are investigated. The effect of a centrally located cutout on the global response is also studied. The analysis is carried out within the framework of the extended finite element method. A Heaviside function is used to capture the jump in the displacement and an enriched shear flexible 4-noded quadrilateral element is used for the spatial discretization. The formulation takes into account the transverse shear deformation and accounts for the lamina material properties at elevated moisture concentrations and temperature. The influence of the plate geometry, the geometry of the cutout, the moisture concentration, the thermal gradient and the boundary conditions on the free flexural vibration is numerically studied.

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Buckling analysis of laminated composite plates with an elliptical/circular cutout using FEM

Cited by 94 publications

References 12 publications

Effect of Various Cut-Out on Buckling Analysis of Laminated Composite Plate Using Fe Simulation

Effect of Various Cut-Out on Buckling Analysis of Laminated Composite Plate Using Fe Simulation

Linear Buckling behaviour of Composite Laminate [(θ/-θ)] with various shaped cutout using FEM

Hygrothermal effects on the free vibration and buckling of laminated composites with cutouts

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