A theoretical study is performed to optimize the design of symmetrically laminated plates with respect to fiber orientation and layer thickness. Rectangular plates simply supported along the edges and with transverse pressure load are considered. The expression for plate flexural stiffness is obtained using approximate energy approaches, such as Ritz-Rayleigh method, using different shape functions. Results of analytical solution are compared with results from finite element analysis, which show a good correlation between theoretical and numerical results. Optimality criteria are applied to the analytical expression of flexural stiffness to determine the optimality condition. A closed form solution is obtained for the fiber orientation and ...
In this study, a lamination parameter based optimization algorithm is developed in a finite element ...
This work deals with the stiffness maximization of laminate plates and tubes from only one point of ...
Mechanical properties of fiber-reinforced laminated composite materials are direction-ally dependent...
[[abstract]]The task of designing symmetric laminated beams with optimal stiffness and damping is co...
In this paper we consider the maximal stiffness design of laminated plates subjected to single and m...
Abstract: Some simple exact solutions for the design of flexural properties of laminates are given;...
The new optimization method for fiber orientation angle optimization of symmetrical multilayer plate...
This paper aims to express the relation of a measure of laminate plate stiffness with respect to the...
Any two-dimensional plate theory is an approximation of the real three-dimen- sional elasticity pro...
Deflection of simply supported laminated composite plate under transverse load is found out by semi-...
AbstractA layerwise optimization (LO) approach is extended to accommodate the finite element analysi...
Mechanical properties of fiber-reinforced laminated composite materials are directionally dependent....
The paper is specialized in optimizing of elastic constants. The first part is devoted to methodolog...
The problems of shape, material, sizing and topology optimization are formulated and solved for thin...
The demand for efficient lightweight structures grows rapidly in the aerospace sector. Topology opti...
In this study, a lamination parameter based optimization algorithm is developed in a finite element ...
This work deals with the stiffness maximization of laminate plates and tubes from only one point of ...
Mechanical properties of fiber-reinforced laminated composite materials are direction-ally dependent...
[[abstract]]The task of designing symmetric laminated beams with optimal stiffness and damping is co...
In this paper we consider the maximal stiffness design of laminated plates subjected to single and m...
Abstract: Some simple exact solutions for the design of flexural properties of laminates are given;...
The new optimization method for fiber orientation angle optimization of symmetrical multilayer plate...
This paper aims to express the relation of a measure of laminate plate stiffness with respect to the...
Any two-dimensional plate theory is an approximation of the real three-dimen- sional elasticity pro...
Deflection of simply supported laminated composite plate under transverse load is found out by semi-...
AbstractA layerwise optimization (LO) approach is extended to accommodate the finite element analysi...
Mechanical properties of fiber-reinforced laminated composite materials are directionally dependent....
The paper is specialized in optimizing of elastic constants. The first part is devoted to methodolog...
The problems of shape, material, sizing and topology optimization are formulated and solved for thin...
The demand for efficient lightweight structures grows rapidly in the aerospace sector. Topology opti...
In this study, a lamination parameter based optimization algorithm is developed in a finite element ...
This work deals with the stiffness maximization of laminate plates and tubes from only one point of ...
Mechanical properties of fiber-reinforced laminated composite materials are direction-ally dependent...