Add to ORKGIn this study, the crack growth behavior and shear stress distribution under typical loading conditions is studied for a composite bonded joint. A novel approach of strain measurement is presented by using a high-resolution digital image correlation system (DIC) which allows detailed investigations of the shear strain distribution within the bondline. By testing 7 different load levels with 3 specimens each in fatigue the crack growth rates, the crack growth threshold and the Paris Law correlation are obtained for an aerospace epoxy adhesive
In tensile test setups strain gauges or extensometers are typically used to measure the strain. Stra...
After a discussion about different models on bonded composite connections reported in the literature...
With the increasing amount of composite materials used for civil aircraft structures, joining and re...
The demand for energy efficient, low weight structures has boosted the use of composite structures a...
Composite primary and secondary aircraft structures have the potential to achieve the same strength ...
Structural bonding and bonded repairs of composite materials become more and more important. Underst...
Adhesive bonding has become a powerful joining technique during the last few decades. It has many ap...
Experimental analysis of the stresses and strains in a glass fibre polymer composite double butt str...
Wrapped composite joint is a novel joining technology which connects steel hollow sections through b...
In the present paper the problem of crack propagation assessment of single lap bonded joints in comp...
This work is the analyse of the results of several test campaigns using the composite fatigue know-...
Adhesive bonding presents many advantages, such as efficient manufacturing and improved structural p...
Fatigue Analysis of Structural Bonded Joints Under Variable Amplitude Loading. For lightweight const...
This study investigates the high loading rate behavior of adhesively bonded carbon/epoxy composite j...
The fatigue crack propagation in adhesively bonded, thick composite joints was investigated experime...
In tensile test setups strain gauges or extensometers are typically used to measure the strain. Stra...
After a discussion about different models on bonded composite connections reported in the literature...
With the increasing amount of composite materials used for civil aircraft structures, joining and re...
The demand for energy efficient, low weight structures has boosted the use of composite structures a...
Composite primary and secondary aircraft structures have the potential to achieve the same strength ...
Structural bonding and bonded repairs of composite materials become more and more important. Underst...
Adhesive bonding has become a powerful joining technique during the last few decades. It has many ap...
Experimental analysis of the stresses and strains in a glass fibre polymer composite double butt str...
Wrapped composite joint is a novel joining technology which connects steel hollow sections through b...
In the present paper the problem of crack propagation assessment of single lap bonded joints in comp...
This work is the analyse of the results of several test campaigns using the composite fatigue know-...
Adhesive bonding presents many advantages, such as efficient manufacturing and improved structural p...
Fatigue Analysis of Structural Bonded Joints Under Variable Amplitude Loading. For lightweight const...
This study investigates the high loading rate behavior of adhesively bonded carbon/epoxy composite j...
The fatigue crack propagation in adhesively bonded, thick composite joints was investigated experime...
In tensile test setups strain gauges or extensometers are typically used to measure the strain. Stra...
After a discussion about different models on bonded composite connections reported in the literature...
With the increasing amount of composite materials used for civil aircraft structures, joining and re...