In this paper an attempt is made to obtain deflections of hybrid, laminated, rectangular and skew composite plates. Analysis is performed by employing the Galerkin technique. Numerical results have been obtained for two types of layups employing Kevlar/epoxy and Boron/epoxy laminae. It is observed that for a given aspect ratio the rigidity of the skew plate increases with an increase in the skew angle. Further, for a specified deflection, the hybrid laminates turn out to be lighter
Most structures are subjected to severe static and dynamic stress, as well as a variety of constrain...
Dynamic Relaxation (DR) method is presented for the geometricallynonlinear laterally loaded, rectang...
In this study, the behaviour of laminated composite plates, fiber Kevlar29, Al2O3powder/epoxy and th...
In this paper an attempt is made to obtain deflections of hybrid, laminated, rectangular and skew co...
In this paper, an attempt is made to obtain the free vibration response of hybrid, laminated rectang...
Deflection of simply supported laminated composite plate under transverse load is found out by semi-...
The convergence and accuracy of the Dynamic Relaxation (DR) solutions for elasticlarge deflection re...
The convergence and accuracy of the Dynamic Relaxation (DR) solutions for elastic large deflection r...
In this study maximum deflection and free vibration of quasi-isotropic thin rectangular plates that ...
Abstract: The present work deals with the modeling and analysis of laminated composites plate. In th...
This paper presents a comparison of theoretical and experimental deflection of a hybrid sandwich pan...
The lowest critical value of the compressive force acting in the plane of symmetrically laminated qu...
95-102The behaviour of a laminated composite skew plate with hole subjected to temperature as well a...
This paper generalizes and extends a numerical formulation within the method to simulate the behavio...
The theoretical analysis depends on the Classical Laminated Plate Theory (CLPT) that is based on the...
Most structures are subjected to severe static and dynamic stress, as well as a variety of constrain...
Dynamic Relaxation (DR) method is presented for the geometricallynonlinear laterally loaded, rectang...
In this study, the behaviour of laminated composite plates, fiber Kevlar29, Al2O3powder/epoxy and th...
In this paper an attempt is made to obtain deflections of hybrid, laminated, rectangular and skew co...
In this paper, an attempt is made to obtain the free vibration response of hybrid, laminated rectang...
Deflection of simply supported laminated composite plate under transverse load is found out by semi-...
The convergence and accuracy of the Dynamic Relaxation (DR) solutions for elasticlarge deflection re...
The convergence and accuracy of the Dynamic Relaxation (DR) solutions for elastic large deflection r...
In this study maximum deflection and free vibration of quasi-isotropic thin rectangular plates that ...
Abstract: The present work deals with the modeling and analysis of laminated composites plate. In th...
This paper presents a comparison of theoretical and experimental deflection of a hybrid sandwich pan...
The lowest critical value of the compressive force acting in the plane of symmetrically laminated qu...
95-102The behaviour of a laminated composite skew plate with hole subjected to temperature as well a...
This paper generalizes and extends a numerical formulation within the method to simulate the behavio...
The theoretical analysis depends on the Classical Laminated Plate Theory (CLPT) that is based on the...
Most structures are subjected to severe static and dynamic stress, as well as a variety of constrain...
Dynamic Relaxation (DR) method is presented for the geometricallynonlinear laterally loaded, rectang...
In this study, the behaviour of laminated composite plates, fiber Kevlar29, Al2O3powder/epoxy and th...
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