The objective of this research was to investigate the fatigue crack growth behavior around the countersunk fastener hole. Both experimental and computational studies were carried out and the results were compared when possible. In the early stage of this research, the fatigue failures at the mechanical joint specimens were investigated and characterized. The three-dimensional finite element analyses revealed that the degree of load transfer through the countersink fastener can influence the cracking behavior at the countersunk fastener hole. This finding was verified by investigating the fracture surfaces of the mechanical joint specimens. The cracking location\u27s dependence on the load transfer can be attributed to the non-uniform bearin...
The cold-expansion process is widely used to enhance the fatigue life of structures with fastener ho...
The cold expansion process is widely used to enhance the fatigue life of structures with fastener ho...
The two historical fuselage failures, Comet in 1954 and Aloha in 1988, illustrate that similar accid...
This research dealt with fatigue cracks that form at countersunk open holes and mainly focused on ob...
This paper focuses on the study and comparison of stress intensity factor solutions for cracks emana...
To understand the different aspects of fatigue behaviour of complex structural joints it will be muc...
Multiple site damage (MSD) is the occurrence of many small cracks at multiple locations such as rive...
Primary aerospace composite structures are commonly assembled with bolted joints due to their abilit...
The main problem investigated is that of the prediction of stress intensity factors and associated f...
In this article, the effect of interference fit on fatigue life of holed plate of mechanical joints ...
The cold expansion technique is often used to introduce beneficial compressive stress at fastener ho...
An investigation of the fatigue crack behavior at fastener holes in a low carbon steel before and af...
An experimental program has been carried out for the evaluation of the influence of the split sleeve...
A modified elastic-plastic finite element program was used to simulate fatigue crack growth and clos...
Stress intensity factor (K) solutions for unsymmetric corner cracks at a straight shank hole subject...
The cold-expansion process is widely used to enhance the fatigue life of structures with fastener ho...
The cold expansion process is widely used to enhance the fatigue life of structures with fastener ho...
The two historical fuselage failures, Comet in 1954 and Aloha in 1988, illustrate that similar accid...
This research dealt with fatigue cracks that form at countersunk open holes and mainly focused on ob...
This paper focuses on the study and comparison of stress intensity factor solutions for cracks emana...
To understand the different aspects of fatigue behaviour of complex structural joints it will be muc...
Multiple site damage (MSD) is the occurrence of many small cracks at multiple locations such as rive...
Primary aerospace composite structures are commonly assembled with bolted joints due to their abilit...
The main problem investigated is that of the prediction of stress intensity factors and associated f...
In this article, the effect of interference fit on fatigue life of holed plate of mechanical joints ...
The cold expansion technique is often used to introduce beneficial compressive stress at fastener ho...
An investigation of the fatigue crack behavior at fastener holes in a low carbon steel before and af...
An experimental program has been carried out for the evaluation of the influence of the split sleeve...
A modified elastic-plastic finite element program was used to simulate fatigue crack growth and clos...
Stress intensity factor (K) solutions for unsymmetric corner cracks at a straight shank hole subject...
The cold-expansion process is widely used to enhance the fatigue life of structures with fastener ho...
The cold expansion process is widely used to enhance the fatigue life of structures with fastener ho...
The two historical fuselage failures, Comet in 1954 and Aloha in 1988, illustrate that similar accid...