Add to ORKGThis article presents numerical simulations of laminates subjected to Compression After Impact (CAI) testing including delamination modelling. Different model of impact damages of laminate were considered. Progressive damage analysis have been employed and different failure criteria have been applied. For each simulation failure load has been estimated as same as the position of damages at destroyed layer. Finally, obtained numerical results were compared with experimental data from referential paper
Delaminations represent a damage mechanisms of paramount interest for composite laminates addressed ...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
Composite materials are assuming a predominant role in structural applications, in particular in aer...
This paper presents a model for the numerical simulation of impact damage, permanent indentation and...
International audienceA numerical approach is presented to estimate the compressive behaviors of 150...
Low-velocity impact damage can drastically reduce the residual mechanical properties of the composit...
The damage tolerance of Carbon Fibre Reinforced Polymer (CFRP) to Barely Visible Impact Damage (BVID...
Today the use of composite materials in the aircraft industry is very widespread also for the primar...
Barely Visible Impact Damage (BVID) can occur when laminated composite material is subject to out-of...
The paper presents recent progress on modelling low velocity impact induced damage in fibre reinforc...
Compression after impact (CAI) is one of the crucial factors affecting material selection and determ...
An efficient numerical approach for the prediction of the Compression After Impact (CAI) strength of...
9 pages, 13 figures.The damage tolerance of various lay-ups of thin carbon/epoxy laminates (1.6–2.2 ...
International audienceThis paper presents a numerical simulation of impact and compression after imp...
Carbon fiber reinforced polymer (CFRP) composites have been widely used in many industrial sectors b...
Delaminations represent a damage mechanisms of paramount interest for composite laminates addressed ...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
Composite materials are assuming a predominant role in structural applications, in particular in aer...
This paper presents a model for the numerical simulation of impact damage, permanent indentation and...
International audienceA numerical approach is presented to estimate the compressive behaviors of 150...
Low-velocity impact damage can drastically reduce the residual mechanical properties of the composit...
The damage tolerance of Carbon Fibre Reinforced Polymer (CFRP) to Barely Visible Impact Damage (BVID...
Today the use of composite materials in the aircraft industry is very widespread also for the primar...
Barely Visible Impact Damage (BVID) can occur when laminated composite material is subject to out-of...
The paper presents recent progress on modelling low velocity impact induced damage in fibre reinforc...
Compression after impact (CAI) is one of the crucial factors affecting material selection and determ...
An efficient numerical approach for the prediction of the Compression After Impact (CAI) strength of...
9 pages, 13 figures.The damage tolerance of various lay-ups of thin carbon/epoxy laminates (1.6–2.2 ...
International audienceThis paper presents a numerical simulation of impact and compression after imp...
Carbon fiber reinforced polymer (CFRP) composites have been widely used in many industrial sectors b...
Delaminations represent a damage mechanisms of paramount interest for composite laminates addressed ...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
Composite materials are assuming a predominant role in structural applications, in particular in aer...