Add to ORKGTo measure the interlaminar fracture toughness and establish delamination failure criteria at room temperature/dry conditions for Carbon fiber reinforced plastics (CFRP). CFRP materials fabricated through two different processing techniques are considered in this study viz., Autoclave molding (AS4/914 Prepreg) and Vacuum Enhanced Resin Infusion Technology-VERITy (Epolam-2063 polymer resin with Carbon fiber reinforcement)
Mode I interlaminar fracture toughness was investigated for the first time for continuous carbon fi...
This study investigates the mode-II delamination performance of filament-wound unidirectional compos...
On the present work, samples of carbon fiber/epoxy composites with different void levels were fabric...
To measure the interlaminar fracture toughness and establish delamination failure criteria at room t...
The objective of this study is to investigate the behavior of the unidirectional CFRP composites sub...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
A method is described to characterize the uniformity of interlaminar fracture toughness of laminated...
The focus of this thesis is to develop methods to predict the damage response of CarbonFibre Reinfor...
Accurate determination of mode III interlaminar fracture toughness is paramount in composite materia...
The Mode I and Mode II fracture behaviour of three carbon-epoxy composite laminates with different f...
A 2/2 twill weave fabric carbon fibre reinforced epoxy matrix composite MTM56/CF0300 was used to inv...
Carbon fiber composites have been increasingly used in aerospace, military, sports, automotive and o...
The work describes the preparation and physicalmechanical characterization of unidirectional CFRP pa...
This paper describes an experimental study developed to characterize the mode I and mode II fractur...
The bond between a fibre and the matrix is very important for the mechanical behaviour of CFRP. The ...
Mode I interlaminar fracture toughness was investigated for the first time for continuous carbon fi...
This study investigates the mode-II delamination performance of filament-wound unidirectional compos...
On the present work, samples of carbon fiber/epoxy composites with different void levels were fabric...
To measure the interlaminar fracture toughness and establish delamination failure criteria at room t...
The objective of this study is to investigate the behavior of the unidirectional CFRP composites sub...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
A method is described to characterize the uniformity of interlaminar fracture toughness of laminated...
The focus of this thesis is to develop methods to predict the damage response of CarbonFibre Reinfor...
Accurate determination of mode III interlaminar fracture toughness is paramount in composite materia...
The Mode I and Mode II fracture behaviour of three carbon-epoxy composite laminates with different f...
A 2/2 twill weave fabric carbon fibre reinforced epoxy matrix composite MTM56/CF0300 was used to inv...
Carbon fiber composites have been increasingly used in aerospace, military, sports, automotive and o...
The work describes the preparation and physicalmechanical characterization of unidirectional CFRP pa...
This paper describes an experimental study developed to characterize the mode I and mode II fractur...
The bond between a fibre and the matrix is very important for the mechanical behaviour of CFRP. The ...
Mode I interlaminar fracture toughness was investigated for the first time for continuous carbon fi...
This study investigates the mode-II delamination performance of filament-wound unidirectional compos...
On the present work, samples of carbon fiber/epoxy composites with different void levels were fabric...