Thermal Buckling and Postbuckling of Symmetrically Laminated Composite Plates

Meyers, C. A.; Hyer, M. W.

doi:10.1080/01495739108927083

Cited by 103 publications

(33 citation statements)

References 3 publications

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“…(22), and these equations are three partial differential equation in terms of the rotation functions (ψ x and ψ y ) and the transverse displacement (w) only. In other words, Eq.…”

Section: The Governing Stability Equations and Their Decoupled Formmentioning

confidence: 99%

“…To find the critical buckling temperature, the prebuckling thermal forces should be found. Thus, solving the membrane form of the equilibrium equations and using the method developed by Meyers and Hyer [22], the prebuckling force resultants of FG plate exposed to the nonuniform temperature distribution across the thickness are found to be [1,3,6,11] N 0…”

Section: Thermal Buckling Analysismentioning

confidence: 99%

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Thermoelastic buckling behavior of thick functionally graded rectangular plates

Bodaghi

Saidi

2011

Arch Appl Mech

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Thermoelastic buckling behavior of thick rectangular plate made of functionally graded materials is investigated in this article. The material properties of the plate are assumed to vary continuously through the thickness of the plate according to a power-law distribution. Three types of thermal loading as uniform temperature raise, nonlinear and linear temperature distribution through the thickness of plate are considered. The coupled governing stability equations are derived based on the Reddy's higher-order shear deformation plate theory using the energy method. The resulted stability equations are decoupled and solved analytically for the functionally graded rectangular plates with two opposite edges simply supported subjected to different types of thermal loading. A comparison of the present results with those available in the literature is carried out to establish the accuracy of the presented analytical method. The influences of power of functionally graded material, plate thickness, aspect ratio, thermal loading conditions and boundary conditions on the critical buckling temperature of aluminum/alumina functionally graded rectangular plates are investigated and discussed in detail. The critical buckling temperatures of thick functionally graded rectangular plates with various boundary conditions are reported for the first time and can be served as benchmark results for researchers to validate their numerical and analytical methods in the future.

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“…(22), and these equations are three partial differential equation in terms of the rotation functions (ψ x and ψ y ) and the transverse displacement (w) only. In other words, Eq.…”

Section: The Governing Stability Equations and Their Decoupled Formmentioning

confidence: 99%

Section: Thermal Buckling Analysismentioning

confidence: 99%

Thermoelastic buckling behavior of thick functionally graded rectangular plates

Bodaghi

Saidi

2011

Arch Appl Mech

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show abstract

“…Sun and Hsu [7] applied classical Kirchhoff deformation theory with the inclusion of transverse shear deformation to the buckling of laminated composite plates due to temperature changes. The thermal buckling and post-buckling response of symmetrically laminated composite plates was investigated by Mayers and Hyer [8] using the Rayleigh-Ritz method. Abramovich [9] investigated the thermal buckling of symmetric and non-symmetric cross-ply composite laminated beams with various boundary conditions based on Timoshenko type equations and first-order shear deformation theory.…”

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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“…Extensive investigations on the thermal bending and post-buckling of isotropic and composite plates and shells were carried out by Tauchert and Huang (1987); Tauchert (1991); Meyers and Hyer (1991) and Leissa (1992), etc. Wu and his colleagues also have established a number of 3D solutions of thermoelastic, dynamic and buckling problems of laminated composite doubly curved and conical shells (Wu et al, 1996a(Wu et al, , 1996bChiu, 2001, 2002) …”

Section: Three-dimensional Elasticity Theorymentioning

confidence: 99%