Composite materials are widely used in various industries because of their distinct properties. Hybridization is an efficient way of designing composite panels to decrease the cost and/or weight while maintaining stiffness properties. In this study, an accurate and efficient framework is developed to optimize laminated sandwich panels composed of high-stiffness face sheets and low-stiffness core. The stiffness properties of face sheets and core are represented using lamination parameters. The governing equations are derived following first-order shear deformation theory and solved using the spectral Chebyshev approach. In multi-objective optimization problems, genetic algorithm is used to determine Pareto-optimal solutions for fundamental f...
This work deals with the problem of the optimum design of a sandwich panel. The design strategy that...
This paper presents results of a study that focuses on developing a genetic algorithm (GA) for multi...
This work deals with the problem of the optimum design of a sandwich structure composed of two lamin...
Producing a light structure with relatively affordable cost without sacrificing strength has always ...
The paper deals with design optimization of sandwich structure made of laminate outer layers and PU...
Composite sandwich panels with honeycomb, corrugated, tetrahedral, trapezoidal, 3D periodic and hybr...
Composite sandwich panels with honeycomb, corrugated, tetrahedral, trapezoidal, 3D periodic and hybr...
A genetic algorithm-based method is proposed to globally optimize the stacking sequence of multi-san...
A method was presented for multi-objective optimization of material distribution of simply supported...
grantor: University of TorontoMinimum weight design is an important criterion in aircraft ...
Composite materials are combinations of, at least, two organic or inorganic materials, working to-ge...
The sandwich material presents a certain interest in term of rigidity and specific resistance for th...
This paper presents an approach for optimizing practical commercial-scale aircraft wings using sandw...
three population-based optimization techniques for the design of composite sandwich materials CW Hud...
This paper presents an approach for optimizing practical commercial-scale aircraft wings using sandw...
This work deals with the problem of the optimum design of a sandwich panel. The design strategy that...
This paper presents results of a study that focuses on developing a genetic algorithm (GA) for multi...
This work deals with the problem of the optimum design of a sandwich structure composed of two lamin...
Producing a light structure with relatively affordable cost without sacrificing strength has always ...
The paper deals with design optimization of sandwich structure made of laminate outer layers and PU...
Composite sandwich panels with honeycomb, corrugated, tetrahedral, trapezoidal, 3D periodic and hybr...
Composite sandwich panels with honeycomb, corrugated, tetrahedral, trapezoidal, 3D periodic and hybr...
A genetic algorithm-based method is proposed to globally optimize the stacking sequence of multi-san...
A method was presented for multi-objective optimization of material distribution of simply supported...
grantor: University of TorontoMinimum weight design is an important criterion in aircraft ...
Composite materials are combinations of, at least, two organic or inorganic materials, working to-ge...
The sandwich material presents a certain interest in term of rigidity and specific resistance for th...
This paper presents an approach for optimizing practical commercial-scale aircraft wings using sandw...
three population-based optimization techniques for the design of composite sandwich materials CW Hud...
This paper presents an approach for optimizing practical commercial-scale aircraft wings using sandw...
This work deals with the problem of the optimum design of a sandwich panel. The design strategy that...
This paper presents results of a study that focuses on developing a genetic algorithm (GA) for multi...
This work deals with the problem of the optimum design of a sandwich structure composed of two lamin...