Add to ORKGOptimisation of thin-walled fibre composite cylindrical shell structures loaded by axial compression is considered, formulated as single objective problem with maximization of the buckling load only, and as multiobjective optimisation with maximization of the buckling load and at the same time minimization of imperfection sensitivity
Fibre-reinforced composites are used in many engineering structures with cylindrical panels being a ...
This paper focuses on criterion functions for gradient based optimization of the buckling load of la...
In this paper some basic questions on optimisation of structures prone to instability behaviour are ...
grantor: University of TorontoOptimal buckling loads of structures subjected to uncertain ...
Thin-walled cylindrical shells are nowadays widely used for principal structures in the aerospace fi...
The object of the presentation is the development of a topology optimization tool for designing fibr...
AbstractNonlinear buckling optimization is introduced as a method for doing laminate optimization on...
Robust design of laminated composite structures is considered in this work. Because laminated compos...
Additive manufacturing for fibre-reinforced composite structures is rapidly diffusing, since it enab...
Robust buckling optimal design of laminated composite structures is conducted in this work. Optimal ...
Thin-walled cylindrical shell components are widely used in engineering and in many cases are expose...
Automated fibre placement (AFP) machines are able to place simultaneously several bundles of fibres,...
Launch-vehicle primary structures like cylindrical shells are increasingly being built as monolithic...
With the introduction of composite materials in the engineering field, the need for improved and che...
This thesis deals with the search for innovative composite solutions for mass reduction of aeronauti...
Fibre-reinforced composites are used in many engineering structures with cylindrical panels being a ...
This paper focuses on criterion functions for gradient based optimization of the buckling load of la...
In this paper some basic questions on optimisation of structures prone to instability behaviour are ...
grantor: University of TorontoOptimal buckling loads of structures subjected to uncertain ...
Thin-walled cylindrical shells are nowadays widely used for principal structures in the aerospace fi...
The object of the presentation is the development of a topology optimization tool for designing fibr...
AbstractNonlinear buckling optimization is introduced as a method for doing laminate optimization on...
Robust design of laminated composite structures is considered in this work. Because laminated compos...
Additive manufacturing for fibre-reinforced composite structures is rapidly diffusing, since it enab...
Robust buckling optimal design of laminated composite structures is conducted in this work. Optimal ...
Thin-walled cylindrical shell components are widely used in engineering and in many cases are expose...
Automated fibre placement (AFP) machines are able to place simultaneously several bundles of fibres,...
Launch-vehicle primary structures like cylindrical shells are increasingly being built as monolithic...
With the introduction of composite materials in the engineering field, the need for improved and che...
This thesis deals with the search for innovative composite solutions for mass reduction of aeronauti...
Fibre-reinforced composites are used in many engineering structures with cylindrical panels being a ...
This paper focuses on criterion functions for gradient based optimization of the buckling load of la...
In this paper some basic questions on optimisation of structures prone to instability behaviour are ...