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Prediction of ship bulkhead deflection under internal explosion. [PDF]
Chen QH, Tao YG, Liang ZG.
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In this chapter we consider a first order shear deformation theory for the static, free vibration and buckling analysis of laminated plates. We introduce a computation of the shear correction factor and solve some examples with MATLAB codes. The main difference between the present chapter and the previous one related to Mindlin plates is that due ...
Ferreira A. J. M., Fantuzzi N.
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Laminated plate theories and fracture of laminated glass plate – A review
Engineering Fracture Mechanics, 2017Abstract The designed fracture of laminated glass (LG) makes it useful for architectural, glazing, automotive safety, photovoltaic, ultraviolet ray protection, and decorative applications. The present review is divided into three sections: the first section includes a description and classification of the laminated plate (LP) theories that are used ...
Ajitanshu Vedrtnam, S.J. Pawar
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Flexure of laminated Reissner plates
9th Aerospace Sciences Meeting, 1971An analysis of the flexure of two isotropic Reissner flat plates, bonded by a thin adhesive layer having finite transverse normal, as well as shear flexibility, is presented. Equations governing the stress distribution in the adhesive are developed in general tensor form. Allowance for different surface shear and normal tractions is provided.
DAVID N. HUTULA, DONALD G. LEMKE
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Journal of Applied Mechanics, 1971
A two-dimensional theory for laminated plates is deduced from the three-dimensional continuum theory for a laminated medium. Plate-stress equations of motion, plate-stress-strain relations, boundary conditions, and plate-displacement equations of motion are presented.
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A two-dimensional theory for laminated plates is deduced from the three-dimensional continuum theory for a laminated medium. Plate-stress equations of motion, plate-stress-strain relations, boundary conditions, and plate-displacement equations of motion are presented.
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Plasticity Analysis of Laminated Composite Plates
Journal of Applied Mechanics, 1982Elastic-plastic behavior of symmetric metal-matrix composite laminates is analyzed for the case of in-plane mechanical loading. The overall response of the laminate at each instant is derived from the elastic-plastic deformation of the individual fibrous layers, and from their mutual constraints.
Bahei-El-Din, Y. A., Dvorak, G. J.
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Dynamic Response of Laminated Composite Plates
AIAA Journal, 1975HE classical method of separation of variables combined with the Mindlin-Goodman procedure1 is employed to analyze the dynamic response of an infinitely long simplysupported composite plate under a uniform dynamic pressure, P0, on the upper surface of the plate.
Sun, Chang-Tsan +2 more
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Damping Characteristics of Laminated Thick Plates
Journal of Applied Mechanics, 1997We develop the analysis for the exact three-dimensional viscoelastic solution for simply supported, thick multilayered composite plate strips. Each layer is assumed to possess monoclinic or higher material symmetry and to be perfectly bonded to adjacent layers.
Taylor, T. W., Nayfeh, A. H.
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