Thermal buckling of shear-deformable composite laminated plates by the spline finite strip method

Dawe, D.J.; Ge, Y.S.

doi:10.1016/s0045-7825(99)00266-2

Cited by 28 publications

(16 citation statements)

References 18 publications

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“…In contrast, there have been fewer investigations for the thermal postbuckling of composite laminated plates [12,13]. The problem of buckling under thermo-mechanical loading has been considered by relatively few investigators [14][15][16]. The analysis of the buckling and postbuckling behavior of isotropic or composite laminated shells is a topic of considerable technical importance in number of branches of engineering.…”

Section: Introductionmentioning

confidence: 99%

Buckling and postbuckling behavior of shell type structures under thermo mechanical loads

Vasic

Maksimović²,

Maksimović³

et al. 2021

THERM SCI

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The thermomechanical buckling and postbuckling behavior of layered composite shell type structure are considered with the finite element method (FEM) under the combination of temperature load and applied mechanical loads. To account for through-thickness shear deformation effects, the thermal elastic, Higher-Order Shear deformation Theory (HOST) is used in this study. The refined higher order theories, that takes into account the effect of transverse normal deformation, is used to develop discrete finite element models for the thermal buckling analysis of composite laminates. Attention in this study is focused on analyzing the temperature effects on buckling and postbuckling behavior of thin shell structural components. Special attention in this paper is focused on studying of values of the hole in curved panel on thermal buckling behavior and consequently to expend and upgrade previously conducted investigation. Using FEM, a broader observation of the critical temperature of loss of stability depending on the size of the hole was conducted. The presented numerical results based on HOST can be used as versatile and accurate method for buckling and postbuckling analyzes of thin-walled laminated plates under thermo-mechanical loads.

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Section: Introductionmentioning

confidence: 99%

Buckling and postbuckling behavior of shell type structures under thermo mechanical loads

Vasic

Maksimović²,

Maksimović³

et al. 2021

THERM SCI

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“…Many investigations on thermally induced behaviors of composite plates are concerned with the thermal stability and vibration. The critical buckling temperatures of laminated plates based on a finite strip method were studied by Dawe and Ge [1]. In the pre-buckling stage, an in-plane thermal stress analysis was conducted first, and a buckling analysis was followed using the determined in-plane stress distribution.…”

Section: Introductionmentioning

confidence: 99%

Thermally induced stability and vibration of initially stressed laminated composite plates

Chen¹,

Chen

Lin³

2016

mech

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“…Thermal buckling analysis of cross-ply laminates is also studied by Mannini [9] using the first-order shear deformation theory and the Rayleigh-Ritz method. Dawe and Ge [10] presented the results for thermally loaded shear deformable composite laminates using the spline finite strip method. Yettram and Brawn [11] predicted the buckling of square perforated plates under biaxial loadings using a direct matrix method.…”

Section: Introductionmentioning

confidence: 99%

Thermal Buckling of Rectangular Laminated Plates with a Hole

Avcı

Kaya

Dağhan

2005

Journal of Reinforced Plastics and Composites

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Thermal buckling analysis of symmetric and antisymmetric laminated composite plates with clamped and simply supported edges, and containing a hole is presented in this paper. The first-order shear deformation theory in conjunction with the variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used to find thermal buckling temperatures of isotropic, glass-epoxy and boron-epoxy laminates. The effects of hole size, angle of ply orientation, lay-up sequences, and boundary conditions on thermal buckling temperatures are investigated. The result is shown in graphical forms for various boundary conditions.

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Thermal buckling of shear-deformable composite laminated plates by the spline finite strip method

Cited by 28 publications

References 18 publications

Buckling and postbuckling behavior of shell type structures under thermo mechanical loads

Buckling and postbuckling behavior of shell type structures under thermo mechanical loads

Thermally induced stability and vibration of initially stressed laminated composite plates

Thermal Buckling of Rectangular Laminated Plates with a Hole

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