The reactivity and processability of prepregs for high performance composites have been investigated as a function of time and storing conditions. The study has been focused on the stability of epoxy matrix carbon fiber prepregs, affected by exposure to controlled environmental conditions before their use in composite manufacturing. Effects of the aging on glass transition temperature, reactivity and processability have been investigated by calorimetry. Dynamic, isothermal and cure simulating tests have been performed to this aim. Results on toughened TGDDMDDS epoxy matrix prepregs are reported. A theoretical kinetic model proposed for the unaged system has been adapted for aged prepregs, by properly evaluating the variations of kinetic ...
Ambient cured wet layup carbon fiber reinforced epoxy composites used extensively in the rehabilitat...
The aerospace industry makes extensive use of composite materials in the form of fibre fabrics pre-i...
Different thermal-oxidative environments (70, 130 ℃ and 190 ℃) have important effects on the propert...
The effects of room temperature aging on the subsequent polymerization kinetics of a bismaleimide (...
Thin-skinned organic matrix composites within aeronautical structures are subjected to thermooxidati...
Most of the composite materials that are used in aerospace structures have been manufactured using a...
Thin-skinned organic matrix composites within aeronautical structures are subjected to thermooxidati...
Carbon fiber reinforced polymer composites are widely used in the rehabilitation, repair, and streng...
In this paper the influence of hygrothermal ageing on the chemical composition, as well as the mecha...
Two different carbon/epoxy prepreg materials were characterized and compared using thermal (DSC, TGA...
The present study aims to investigate the effect of thermo-oxidative aging on the mechanical, chemic...
The present paper examines the effects of hygrothermal aging on the reinforced epoxy composites. The...
In this study, four types of carbon fibre-reinforced epoxy samples were exposed to accelerated aging...
Preliminary studies were carried out on the storage life of prepregs made out of bifunctional epoxy ...
ABSTRACT: Studies were carried out on the storage life of Room Temperature (RT)-curable pre-pregs co...
Ambient cured wet layup carbon fiber reinforced epoxy composites used extensively in the rehabilitat...
The aerospace industry makes extensive use of composite materials in the form of fibre fabrics pre-i...
Different thermal-oxidative environments (70, 130 ℃ and 190 ℃) have important effects on the propert...
The effects of room temperature aging on the subsequent polymerization kinetics of a bismaleimide (...
Thin-skinned organic matrix composites within aeronautical structures are subjected to thermooxidati...
Most of the composite materials that are used in aerospace structures have been manufactured using a...
Thin-skinned organic matrix composites within aeronautical structures are subjected to thermooxidati...
Carbon fiber reinforced polymer composites are widely used in the rehabilitation, repair, and streng...
In this paper the influence of hygrothermal ageing on the chemical composition, as well as the mecha...
Two different carbon/epoxy prepreg materials were characterized and compared using thermal (DSC, TGA...
The present study aims to investigate the effect of thermo-oxidative aging on the mechanical, chemic...
The present paper examines the effects of hygrothermal aging on the reinforced epoxy composites. The...
In this study, four types of carbon fibre-reinforced epoxy samples were exposed to accelerated aging...
Preliminary studies were carried out on the storage life of prepregs made out of bifunctional epoxy ...
ABSTRACT: Studies were carried out on the storage life of Room Temperature (RT)-curable pre-pregs co...
Ambient cured wet layup carbon fiber reinforced epoxy composites used extensively in the rehabilitat...
The aerospace industry makes extensive use of composite materials in the form of fibre fabrics pre-i...
Different thermal-oxidative environments (70, 130 ℃ and 190 ℃) have important effects on the propert...