Transverse cracking in cross-ply laminated composite beams is investigated as a function of the level of thermal residual stresses. A range of residual stresses was obtained by varying the lay-up of the beam considered. Carbon-and glass-reinforced polyetherimide was chosen for their capacity to produce high levels of thermal stress. The experimental work focussing on the occurrence of the first transverse crack in 5 types of laminated beam is reported. The data obtained is analysed using both continuum mechanics and fracture mechanics principle. The results show that for this particular case, the first transverse crack can be described with a maximum stress criterion. The authors also suggest that the data obtained can be used to define a c...
This study addresses matrix-dominated failures in carbon fiber/polymer matrix composite laminates in...
Due to the character of the original source materials and the nature of batch digitization, quality ...
In spite of their advantages, e.g. high strength, low weight, and high stiffness, composite laminate...
Delamination along the 0°/90° interface following transverse cracking in the 90° plies of a cross-pl...
An analytical model based on the principle of minimum potential energy is developed and applied to d...
Two different methods of solution are used to study the effects of transverse cracks in cross-ply co...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
This study followed numerous simulations of the stress field distribution in damaged composite cross...
In this paper the progressive transverse ply cracking in [±θm/90n]s composite laminates is investiga...
The results of stress field distribution in damage cross-ply laminates prompt us to elaborate an ene...
Due to the character of the original source materials and the nature of batch digitization, quality ...
By partitioning the total stresses in a damaged composite into either mechanical and residual stress...
Unidirectional glass fibre reinforced epoxy and polyester laminae having a range of fibre contents, ...
This study addresses matrix-dominated failures in carbon fiber/polymer matrix composite laminates in...
Due to the character of the original source materials and the nature of batch digitization, quality ...
In spite of their advantages, e.g. high strength, low weight, and high stiffness, composite laminate...
Delamination along the 0°/90° interface following transverse cracking in the 90° plies of a cross-pl...
An analytical model based on the principle of minimum potential energy is developed and applied to d...
Two different methods of solution are used to study the effects of transverse cracks in cross-ply co...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
This study followed numerous simulations of the stress field distribution in damaged composite cross...
In this paper the progressive transverse ply cracking in [±θm/90n]s composite laminates is investiga...
The results of stress field distribution in damage cross-ply laminates prompt us to elaborate an ene...
Due to the character of the original source materials and the nature of batch digitization, quality ...
By partitioning the total stresses in a damaged composite into either mechanical and residual stress...
Unidirectional glass fibre reinforced epoxy and polyester laminae having a range of fibre contents, ...
This study addresses matrix-dominated failures in carbon fiber/polymer matrix composite laminates in...
Due to the character of the original source materials and the nature of batch digitization, quality ...
In spite of their advantages, e.g. high strength, low weight, and high stiffness, composite laminate...