Add to ORKGInternational audienceCohesive finite elements are used to model impact induced delamination prediction of T800/21M unidirectional laminated composite. DCB, ELS and MMB tests are used to identify cohesive element parameters. Results from experiments and numerical prediction of impact induced delamination by commercially available code LS-DYNA are compared
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
Delamination initiation and propagation of aeronautic composites is an active field of research. In ...
The paper investigates the potential of cohesive interface elements for damage prediction in laminat...
International audienceCohesive finite elements are used to model impact induced delamination predict...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
Cohesive finite elements are used to model impact induced delamination prediction of T800/21M unidir...
International audienceIn this paper we present a methodology for the prediction of impact induced da...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
The implementation of cohesive elements for studying the delamination process in composite laminates...
International audienceWe show that the behavior of T700/M21s and T800/M21s composite panels are affe...
Finite element crash modeling of composite structures is limited by the inability of current commerc...
Finite element crash modeling of composite structures is limited by the inability of current commerc...
Purpose - The purpose of this paper is to assess a numerical tool to simulate and predict the onset ...
Carbon fibre reinforced plastics, though carrying excellent specific properties, present also new an...
International audienceDelamination initiation and propagation of aeronautic composites is an active ...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
Delamination initiation and propagation of aeronautic composites is an active field of research. In ...
The paper investigates the potential of cohesive interface elements for damage prediction in laminat...
International audienceCohesive finite elements are used to model impact induced delamination predict...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
Cohesive finite elements are used to model impact induced delamination prediction of T800/21M unidir...
International audienceIn this paper we present a methodology for the prediction of impact induced da...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
The implementation of cohesive elements for studying the delamination process in composite laminates...
International audienceWe show that the behavior of T700/M21s and T800/M21s composite panels are affe...
Finite element crash modeling of composite structures is limited by the inability of current commerc...
Finite element crash modeling of composite structures is limited by the inability of current commerc...
Purpose - The purpose of this paper is to assess a numerical tool to simulate and predict the onset ...
Carbon fibre reinforced plastics, though carrying excellent specific properties, present also new an...
International audienceDelamination initiation and propagation of aeronautic composites is an active ...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
Delamination initiation and propagation of aeronautic composites is an active field of research. In ...
The paper investigates the potential of cohesive interface elements for damage prediction in laminat...