Add to ORKGMotivation Current shell-element based design tools used in the automotive industry do not allow for failure prediction in complex composite structures. An automated method to identify and analyse structural hot-spots for all potential failure modes is therefore needed
In the current study a high fidelity analysis approach is used to predict the failure process of not...
International audienceThe design and certification process of aerospace structures requires a detail...
The purpose of this work is to propose an innovative global/local approach for the failure onset ana...
In this paper, failure initiation in composite structures due to high out-of-plane load components i...
Analysis of large complex composite structures with state of the art failure initiation criteria is ...
The automotive industry needs to reduce energy consumption to decrease environmental impact. This ca...
In this paper, the potential and limitations to a proposed methodology for finding hot spots in larg...
In this paper, intrabundle failure initiation in NCF reinforced composite materials is predicted bas...
This paper introduces a user-friendly tool for accurate stress prediction in laminate shell models i...
Identifying the hotspots for damage initiation in large-scale composite structure designs presents a...
In aerospace, carbon fibre-reinforced polymer (CFRP) materials and postbuckling skin-stiffened struc...
The prediction of the actual stress fields in real structural applications is still not completely r...
The aerospace industry invests heavily in the design and manufacture of composite materials. Aircraf...
In aerospace, carbon-fiber-reinforced polymer (CFRP) composites and postbuckling skin-stiffened stru...
Composite skin-stiffened structures can withstand significant loads after initial buckling has occur...
In the current study a high fidelity analysis approach is used to predict the failure process of not...
International audienceThe design and certification process of aerospace structures requires a detail...
The purpose of this work is to propose an innovative global/local approach for the failure onset ana...
In this paper, failure initiation in composite structures due to high out-of-plane load components i...
Analysis of large complex composite structures with state of the art failure initiation criteria is ...
The automotive industry needs to reduce energy consumption to decrease environmental impact. This ca...
In this paper, the potential and limitations to a proposed methodology for finding hot spots in larg...
In this paper, intrabundle failure initiation in NCF reinforced composite materials is predicted bas...
This paper introduces a user-friendly tool for accurate stress prediction in laminate shell models i...
Identifying the hotspots for damage initiation in large-scale composite structure designs presents a...
In aerospace, carbon fibre-reinforced polymer (CFRP) materials and postbuckling skin-stiffened struc...
The prediction of the actual stress fields in real structural applications is still not completely r...
The aerospace industry invests heavily in the design and manufacture of composite materials. Aircraf...
In aerospace, carbon-fiber-reinforced polymer (CFRP) composites and postbuckling skin-stiffened stru...
Composite skin-stiffened structures can withstand significant loads after initial buckling has occur...
In the current study a high fidelity analysis approach is used to predict the failure process of not...
International audienceThe design and certification process of aerospace structures requires a detail...
The purpose of this work is to propose an innovative global/local approach for the failure onset ana...