Add to ORKGInterlaminar normal stresses are induced with interlaminar shear stresses leading to mixed-mode delamination (MMD) in curved cross-ply composite laminates. Dynamic mixed-mode delamination is studied using explicit finite element method and Cohesive Zone Modelling Dynamic response of the specimen is compared with the experiments
One of the widely used geometrically complex parts in advanced commercial aircraft is L-shaped compo...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
Curved composite parts are increasingly replacing metal ribs and box structures in recent civil aero...
One of the widely used geometrically complex parts in recent civil passenger aircrafts is the L-shap...
Delamination, or interlaminar debonding, is a commonly observed failure mechanism in composite lamin...
In the wind energy industry, new advances in composite manufacturing technology and high demand for ...
In aerospace and wind energy industries, new advances in composite manufacturing technology and high...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
One of the most common failure modes for laminated composite structures is delamination, or interlam...
The objective of this study is to determine the mixed-mode I+II interlaminar fracture toughness at h...
This work aims at studying the mixed-mode delamination process in Moment-Loaded Double Cantilever Be...
Dynamic delamination in curved composite laminates is investigated experimentally and numerically. T...
A simplified Cohesive Zone Model (CZM) was developed for the analysis of mixed-mode I-II delaminatio...
This work aims at studying the mixed-mode delamination process in Moment-Loaded Double Cantilever Be...
One of the widely used geometrically complex parts in advanced commercial aircraft is L-shaped compo...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
Curved composite parts are increasingly replacing metal ribs and box structures in recent civil aero...
One of the widely used geometrically complex parts in recent civil passenger aircrafts is the L-shap...
Delamination, or interlaminar debonding, is a commonly observed failure mechanism in composite lamin...
In the wind energy industry, new advances in composite manufacturing technology and high demand for ...
In aerospace and wind energy industries, new advances in composite manufacturing technology and high...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
One of the most common failure modes for laminated composite structures is delamination, or interlam...
The objective of this study is to determine the mixed-mode I+II interlaminar fracture toughness at h...
This work aims at studying the mixed-mode delamination process in Moment-Loaded Double Cantilever Be...
Dynamic delamination in curved composite laminates is investigated experimentally and numerically. T...
A simplified Cohesive Zone Model (CZM) was developed for the analysis of mixed-mode I-II delaminatio...
This work aims at studying the mixed-mode delamination process in Moment-Loaded Double Cantilever Be...
One of the widely used geometrically complex parts in advanced commercial aircraft is L-shaped compo...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...