A combined experimental and analytical investigation of an adhesively-bonded composite joint was conducted to characterize the fracture mode dependence of cyclic debonding. The system studied consisted of graphite/epoxy adherends bonded with EC 3445 adhesive. Several types of specimens are tested which provide the cyclic debond growth rate measurements under various load conditions: mode 1, mixed mode 1 to 2, and mostly mode 2. This study shows that the total strain-energy-release rate is the governing factor for cyclic debonding
Strain energy release rates were used to correlate cyclic debonding between metal sheets and composi...
This study investigates the high loading rate behavior of adhesively bonded carbon/epoxy composite j...
The strains at which buckling and debond growth occur in adhesively bonded composite flanges contain...
A combined experimental and analytical investigation of an adhesively bonded composite joint was con...
The fatigue behavior of a simple composite to composite bonded joint was analyzed. The cracked lap s...
A study was undertaken to characterize the debond growth mechanism of adhesively bonded composite jo...
Symmetric and unsymmetric double cantilever beam (DCB) specimens were tested and analyzed to assess ...
The fatigue damage mechanism of composite to composite adhesively bonded joints was characterized. T...
An experimental study of cracked-lap-shear specimens was conducted to determine the influence of adh...
When an adhesively bonded joint is undergoing cyclic loading, one of the possible damage modes that ...
A geometrically nonlinear finite element analysis of cohesive failure in typical joints is presented...
Cyclic debonding rates were measured during constant-amplitude loading of specimens made of graphite...
The objective of this investigation was to characterize the pure mode 1 delamination growth in metal...
The critical strain energy release rates associated with debonding of the adhesive bondlines in grap...
Bonded lap joints were manufactured and tested under static and fatigue loading. Specimens were desi...
Strain energy release rates were used to correlate cyclic debonding between metal sheets and composi...
This study investigates the high loading rate behavior of adhesively bonded carbon/epoxy composite j...
The strains at which buckling and debond growth occur in adhesively bonded composite flanges contain...
A combined experimental and analytical investigation of an adhesively bonded composite joint was con...
The fatigue behavior of a simple composite to composite bonded joint was analyzed. The cracked lap s...
A study was undertaken to characterize the debond growth mechanism of adhesively bonded composite jo...
Symmetric and unsymmetric double cantilever beam (DCB) specimens were tested and analyzed to assess ...
The fatigue damage mechanism of composite to composite adhesively bonded joints was characterized. T...
An experimental study of cracked-lap-shear specimens was conducted to determine the influence of adh...
When an adhesively bonded joint is undergoing cyclic loading, one of the possible damage modes that ...
A geometrically nonlinear finite element analysis of cohesive failure in typical joints is presented...
Cyclic debonding rates were measured during constant-amplitude loading of specimens made of graphite...
The objective of this investigation was to characterize the pure mode 1 delamination growth in metal...
The critical strain energy release rates associated with debonding of the adhesive bondlines in grap...
Bonded lap joints were manufactured and tested under static and fatigue loading. Specimens were desi...
Strain energy release rates were used to correlate cyclic debonding between metal sheets and composi...
This study investigates the high loading rate behavior of adhesively bonded carbon/epoxy composite j...
The strains at which buckling and debond growth occur in adhesively bonded composite flanges contain...