Buckling behaviour of laminated composite structures using a discrete higher-order displacement model

Moita, J.S; Soares, Carlos A. Mota

doi:10.1016/0263-8223(96)00025-6

Cited by 31 publications

(9 citation statements)

References 32 publications

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“…The differential operator matrix [G] and the initial stress matrix [S] of Equation (16) are not given here for the sake of brevity and can be obtained from Moita et al (1996).…”

Section: Element Geometric Stiffness Matrixmentioning

confidence: 99%

“…A detailed review of works on the buckling of moderately thick laminated CYL shells using first and higher-order shear deformation theories was presented by Simitses (1996). Moita et al (1996) studied the buckling behaviour of laminated shells using a discrete higher-order displacement model. Hybrid/ mixed finite element formulation was applied by Gendy et al (1997) to study the vibration and stability behaviour of composite plates and shells.…”

Section: Introductionmentioning

confidence: 99%

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Buckling of laminated composite hypars and conoids using a higher-order theory

Pradyumna

Bandyopadhyay

2010

The IES Journal Part A: Civil & Structural Engineering

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A C 0 finite element formulation using a higher-order shear deformation theory (HSDT) is developed and used to analyse the buckling behaviour of laminated hypar and conoids. Higher order terms in the Taylor's series expansion are used to represent the higher-order transverse cross-sectional deformation modes. The formulation includes Sanders' approximation for doubly curved shells considering the effect of transverse shear. A realistic parabolic distribution of transverse shear strains through the shell thickness is assumed and the use of shear correction factor is avoided. The accuracy of the formulation is validated by carrying out convergence study and comparing the results with those available in the literature.

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“…The differential operator matrix [G] and the initial stress matrix [S] of Equation (16) are not given here for the sake of brevity and can be obtained from Moita et al (1996).…”

Section: Element Geometric Stiffness Matrixmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

Buckling of laminated composite hypars and conoids using a higher-order theory

Pradyumna

Bandyopadhyay

2010

The IES Journal Part A: Civil & Structural Engineering

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“…Putcha and Reddy [22] have presented an analytical solution and finite element method for buckling analysis of laminated plates based on Navier method and by using (HOPT) and (FSDT) plate theory. Moita et al [23] have also developed a finite element method for stability analysis of laminated plates. Jones [24] has studied mechanical behavior of laminated composite plates by using CLPT and an analytical solution.…”

Section: Introductionmentioning

confidence: 99%

Buckling Analysis of Laminated Composite Plates Using Higher Order Semi—Analytical Finite Strip Method

2009

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Rectangular plates made of laminated composite material because of the advantageously high strength and stiffness to weight ratio are used frequently as structural component in various branches of engineering, chief of which are aerospace and marine engineering. Design concepts of these plates that lead to the increase in the buckling load can directly lower the structural cost and/or weight. The finite strip method is one of a number of procedures which can be used to solve the buckling problem of plate structures. In the present work the main concern is with the buckling behavior of plates with simply supported ends subjected to uni-axial pure compression loads. The solution is sought by implementing the higher order semi-analytical finite strip method which incorporates additional degrees of freedom for each nodal line by using Reddy's higher order plate theory. Therefore the current method is more universal in dealing with different plate thicknesses. In addition, in this semi-analytical finite strip method, all the displacements are postulated by the appropriate harmonic shape functions in the longitudinal direction and polynomial interpolation functions in the transverse direction. The solution is based on the concept of principle of minimum potential energy and an eigen-value analysis is subsequently carried out. From the presented results it can be concluded that the higher order semi-analytical finite strip method is very reliable for the preliminary design of composite plates especially in the case of buckling analysis of relatively thick plates.

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“…An eight node isoparametric element with 10 degrees of freedom per node was developed based on higher-order theory to analyze the linear buckling of multilaminated composite plate-shell structures [16]. Shiau and Wu [17] proposed an 72 DOF high precision high-order triangular plate element for analysis of postbuckling behavior of a laminated composite plate.…”

Section: Introductionmentioning

confidence: 99%

Thermal buckling measurement of a laminated composite plate under a uniform temperature distribution using the digital image correlation method

Jin

et al. 2015

Composite Structures

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Buckling behaviour of laminated composite structures using a discrete higher-order displacement model

Cited by 31 publications

References 32 publications

Buckling of laminated composite hypars and conoids using a higher-order theory

Buckling of laminated composite hypars and conoids using a higher-order theory

Buckling Analysis of Laminated Composite Plates Using Higher Order Semi—Analytical Finite Strip Method

Thermal buckling measurement of a laminated composite plate under a uniform temperature distribution using the digital image correlation method

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