The paper deals with the optimisation of dynamic properties of a composite cantilever cylinder. The optimised parameters are both the fundamental natural frequency f1 as well as the gap in frequency space around a selected external excitation force allowing to avoid the resonance phenomenon. The optimisation is performed using a novel approach combining particle swarm optimisation and artificial neural networks. The evolutionary algorithms are used to solve the optimisation problem with many local minima while neural networks are used to substitute time-consuming finite element calculations of the minimisation problem objective function
The aircraft fuselage is idealized as a composite cylinder, its vibro-acoustic properties are studie...
In mechanical and structural systems, resonance may cause large strains and stresses which can lead ...
This paper introduces the design optimization strategies, especially for structures which have dynam...
In this paper, the optimal fiber orientations relative to the principle axis of composite cylindrica...
This paper deals with the definition of a post-buckling optimisation procedure for the design of com...
The structural properties of a composite laminate can be tailored by allowing the fibres to vary the...
The main driver of aerospace structures design is the increase in performances of currently in use c...
This paper deals with the definition of an optimization procedure for the design of composite stiffe...
Structural optimization using computational tools has become a major research field in recent years....
The objective of this paper is to develop a multiple objective optimization procedure for crashworth...
AbstractNeural-Network Response Surfaces (NNRS) is applied to replace the actual expensive finite el...
In this study, the layer optimization was carried out for maximizing the lowest (first) fundamental ...
In this study the layer optimisation was carried out for maximum fundamental frequency of laminated ...
A otimização estrutural, utilizando ferramentas computacionais é um grande campo de pesquisa na atua...
AbstractAn adaptive approximation-based optimization (AABO) procedure is developed for the optimum d...
The aircraft fuselage is idealized as a composite cylinder, its vibro-acoustic properties are studie...
In mechanical and structural systems, resonance may cause large strains and stresses which can lead ...
This paper introduces the design optimization strategies, especially for structures which have dynam...
In this paper, the optimal fiber orientations relative to the principle axis of composite cylindrica...
This paper deals with the definition of a post-buckling optimisation procedure for the design of com...
The structural properties of a composite laminate can be tailored by allowing the fibres to vary the...
The main driver of aerospace structures design is the increase in performances of currently in use c...
This paper deals with the definition of an optimization procedure for the design of composite stiffe...
Structural optimization using computational tools has become a major research field in recent years....
The objective of this paper is to develop a multiple objective optimization procedure for crashworth...
AbstractNeural-Network Response Surfaces (NNRS) is applied to replace the actual expensive finite el...
In this study, the layer optimization was carried out for maximizing the lowest (first) fundamental ...
In this study the layer optimisation was carried out for maximum fundamental frequency of laminated ...
A otimização estrutural, utilizando ferramentas computacionais é um grande campo de pesquisa na atua...
AbstractAn adaptive approximation-based optimization (AABO) procedure is developed for the optimum d...
The aircraft fuselage is idealized as a composite cylinder, its vibro-acoustic properties are studie...
In mechanical and structural systems, resonance may cause large strains and stresses which can lead ...
This paper introduces the design optimization strategies, especially for structures which have dynam...