The fracture resistance, Gc, of adhesively bonded joints is known to vary significantly with loading mode and because joints are usually subject to mixed-mode loading in service, it is essential to be able to partition Gc into its I/II components so the appropriate failure criterion can be derived. Various partitioning schemes have been proposed in the literature but they give different results and which is most suitable has been an open question. In this work, joints were tested under a wide range of I/II loading ratios and the various partition schemes were assessed. The singular and global schemes were found to define the extremes, while Davidson’s non-singular field scheme represents an intermediate case. The semi-analytical scheme prop...
Fiber-reinforced polymer (FRP) composites are increasingly used in many load-bearing structures. Jo...
Until now, some test specimens with different shapes and loading mechanisms have been utilized for i...
Adhesive bonding has been increasingly used for part manufacturing and repair of composite aircraft ...
The natural ability to join different materials is one of the main advantages of adhesive joints. It...
AbstractUp to now the failure load assessment of bonded joints is still not fully understood. This w...
The dissemination of composite materials introduces applications of hybrid structures with composite...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering."Dec...
69 p.The study of interface strength in bonded materials particularly in joints is of practical inte...
The dissemination of composite materials introduces applications of hybrid structures with composite...
ABSTRACT: The study focuses on using fracture mechanics to evaluate mixed-mode fracture properties...
grantor: University of TorontoThe thesis presents a new experimental method for fracture t...
grantor: University of TorontoThe thesis presents a new experimental method for fracture t...
Abstract This work is concerned with the analysis of failure of adhesive joints. Typically adhesive ...
The mixed-mode fatigue and fracture behaviors of adhesively-bonded pultruded glass fiber-reinforced ...
It has been widely reported that the delamination toughness of adhesive joints and polymer matrix co...
Fiber-reinforced polymer (FRP) composites are increasingly used in many load-bearing structures. Jo...
Until now, some test specimens with different shapes and loading mechanisms have been utilized for i...
Adhesive bonding has been increasingly used for part manufacturing and repair of composite aircraft ...
The natural ability to join different materials is one of the main advantages of adhesive joints. It...
AbstractUp to now the failure load assessment of bonded joints is still not fully understood. This w...
The dissemination of composite materials introduces applications of hybrid structures with composite...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering."Dec...
69 p.The study of interface strength in bonded materials particularly in joints is of practical inte...
The dissemination of composite materials introduces applications of hybrid structures with composite...
ABSTRACT: The study focuses on using fracture mechanics to evaluate mixed-mode fracture properties...
grantor: University of TorontoThe thesis presents a new experimental method for fracture t...
grantor: University of TorontoThe thesis presents a new experimental method for fracture t...
Abstract This work is concerned with the analysis of failure of adhesive joints. Typically adhesive ...
The mixed-mode fatigue and fracture behaviors of adhesively-bonded pultruded glass fiber-reinforced ...
It has been widely reported that the delamination toughness of adhesive joints and polymer matrix co...
Fiber-reinforced polymer (FRP) composites are increasingly used in many load-bearing structures. Jo...
Until now, some test specimens with different shapes and loading mechanisms have been utilized for i...
Adhesive bonding has been increasingly used for part manufacturing and repair of composite aircraft ...