This thesis aims to develop a computational scheme for simultaneous sizing, layout and topology optimization for buckling and postbuckling of stiffened panels. Many efforts have been made using structural optimization techniques to improve the buckling and postbuckling behaviours of stiffened panels, focusing on sizing and layout optimization. Stiffener internal topologies have however, received little attention for optimization. This reduces the design space that can be searched, and consequently limits the potential improvement in structural performance. In this thesis, a level-set-based topology optimization parameterization is developed, enabling the simultaneous optimization of the thicknesses of the skin and stiffeners,...
In this paper, a topology optimization methodology for the minimum weight of the composite stiffened...
Stiffened panels with curved stiffeners have shown a potential for structural tailoring of metallic ...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...
This thesis aims to develop a computational scheme for simultaneous sizing, layout and topology op...
This thesis aims to develop a computational scheme for simultaneous sizing, layout and topology op...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
This study investigates the weight minimization of stiffened panels simultaneously optimizing size, ...
This study investigates the weight minimization of stiffened panels simultaneously optimizing size, ...
Simultaneous layout and topology optimization of stiffened panels is investigated in this paper usin...
Simultaneous layout and topology optimization of stiffened panels is investigated in this paper usin...
Simultaneous layout and topology optimization of stiffened panels is investigated in this paper by a...
In this paper, an innovative design methodology is proposed to simultaneously optimize the size, lay...
The design of stiffeners is an effective approach to enhance the stiffness of panel-type structures....
In this paper, a topology optimization methodology for the minimum weight of the composite stiffened...
Stiffened panels with curved stiffeners have shown a potential for structural tailoring of metallic ...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...
This thesis aims to develop a computational scheme for simultaneous sizing, layout and topology op...
This thesis aims to develop a computational scheme for simultaneous sizing, layout and topology op...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
This study investigates the weight minimization of stiffened panels simultaneously optimizing size, ...
This study investigates the weight minimization of stiffened panels simultaneously optimizing size, ...
Simultaneous layout and topology optimization of stiffened panels is investigated in this paper usin...
Simultaneous layout and topology optimization of stiffened panels is investigated in this paper usin...
Simultaneous layout and topology optimization of stiffened panels is investigated in this paper by a...
In this paper, an innovative design methodology is proposed to simultaneously optimize the size, lay...
The design of stiffeners is an effective approach to enhance the stiffness of panel-type structures....
In this paper, a topology optimization methodology for the minimum weight of the composite stiffened...
Stiffened panels with curved stiffeners have shown a potential for structural tailoring of metallic ...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...