'Torayca' T800H/3900-2 is the first material qualified on Boeing Material Specification (BMS 8-276) which utilizes the thermoplastic-particulate interlayer toughening technology. Two manufacturing processes, the autoclave process and the fast heating rated Quickstep™ process, were employed to cure this material. The Quickstep process is a unique composite production technology which utilizes the fast heat transfer rate of fluid to heat and cure polymer composite components. The manufacturing influence on the mode I delamination fracture toughness of laminates was investigated by performing double cantilever beam tests. The composite specimens fabricated by two processes exhibited dissimilar delamination resistance curves (R-curves) un...
Interlaminar fracture is a dominant mode of failure in advanced composite materials. The resistance ...
Inter-laminar fracture toughness is an important parameter to characterize the delamination propagat...
This paper addresses the characterisation of the mode I interlaminar fracture toughness of a carbon ...
'Torayca' T800H/3900-2 is the first material qualified on Boeing Material Specification (B...
Mode I interlaminar fracture toughness was investigated for the first time for continuous carbon fi...
A 2/2 twill weave fabric carbon fibre reinforced epoxy matrix composite MTM56/CF0300 was used to inv...
The experimental investigation of fracture toughness under Mode I loading conditions have been perfo...
In this work the Mode I fracture toughness behavior of unidirectional CFRP laminates is investigated...
Mode Ⅱ interlaminar fracture toughness is an indispensable mechanical performance parameter for dama...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
The use of composite materials in primary aerospace structures is continually increasing due to thei...
Carbon fibre reinforced thermoset composites make for lighter and stronger structures and are widely...
A popular approach to the characterisation of the propagation of interlaminar cracks has been throug...
An automated fibre placement method has been developed to build through-thickness reinforcement into...
To measure the interlaminar fracture toughness and establish delamination failure criteria at room t...
Interlaminar fracture is a dominant mode of failure in advanced composite materials. The resistance ...
Inter-laminar fracture toughness is an important parameter to characterize the delamination propagat...
This paper addresses the characterisation of the mode I interlaminar fracture toughness of a carbon ...
'Torayca' T800H/3900-2 is the first material qualified on Boeing Material Specification (B...
Mode I interlaminar fracture toughness was investigated for the first time for continuous carbon fi...
A 2/2 twill weave fabric carbon fibre reinforced epoxy matrix composite MTM56/CF0300 was used to inv...
The experimental investigation of fracture toughness under Mode I loading conditions have been perfo...
In this work the Mode I fracture toughness behavior of unidirectional CFRP laminates is investigated...
Mode Ⅱ interlaminar fracture toughness is an indispensable mechanical performance parameter for dama...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
The use of composite materials in primary aerospace structures is continually increasing due to thei...
Carbon fibre reinforced thermoset composites make for lighter and stronger structures and are widely...
A popular approach to the characterisation of the propagation of interlaminar cracks has been throug...
An automated fibre placement method has been developed to build through-thickness reinforcement into...
To measure the interlaminar fracture toughness and establish delamination failure criteria at room t...
Interlaminar fracture is a dominant mode of failure in advanced composite materials. The resistance ...
Inter-laminar fracture toughness is an important parameter to characterize the delamination propagat...
This paper addresses the characterisation of the mode I interlaminar fracture toughness of a carbon ...