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From thin to extra-thick adhesive layer thicknesses: Fracture of bonded joints under mode I loading conditions
From thin to extra-thick adhesive layer thicknesses: Fracture of bonded joints under mode I loading conditions
On the physics of applying finite width and geometry correction factors in fatigue crack growth predictions of GLARE
On the physics of applying finite width and geometry correction factors in fatigue crack growth predictions of GLARE
A Roadmap for developing an Industrial Continuous Ultrasonic Welding Process for Thermoplastic Composites
A Roadmap for developing an Industrial Continuous Ultrasonic Welding Process for Thermoplastic Composites
Structural health monitoring data fusion for in-situ life prognosis of composite structures
Structural health monitoring data fusion for in-situ life prognosis of composite structures
Theoretical analysis of fatigue failure in mechanically fastened Fibre Metal Laminate joints containing multiple cracks
Theoretical analysis of fatigue failure in mechanically fastened Fibre Metal Laminate joints containing multiple cracks
Design and Experimental Assessment of a Multi-spherical Composite- Overwrapped Pressure Vessel for Cryogenic Storage
Design and Experimental Assessment of a Multi-spherical Composite- Overwrapped Pressure Vessel for Cryogenic Storage
Towards robust sequential ultrasonic spot welding of thermoplastic composites
Towards robust sequential ultrasonic spot welding of thermoplastic composites: Welding process control strategy for consistent weld quality
Fatigue crack surface area and crack front length
Fatigue crack surface area and crack front length: New ways to look at fatigue crack growth
The stress ratio effect on plastic dissipation during fatigue crack growth
The stress ratio effect on plastic dissipation during fatigue crack growth
Towards a physics-based relationship for crack growth under different loading modes
Towards a physics-based relationship for crack growth under different loading modes
Using acoustic emission to understand fatigue crack growth within a single load cycle
Using acoustic emission to understand fatigue crack growth within a single load cycle
Analytical solutions for crack opening displacements of eccentric cracks in thin-walled metallic plates
Analytical solutions for crack opening displacements of eccentric cracks in thin-walled metallic plates
Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring
Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring
Incorporating Inductive Bias into Deep Learning
Incorporating Inductive Bias into Deep Learning: A Perspective from Automated Visual Inspection in Aircraft Maintenance
Carbon fiber-reinforced polymer pultrusions adhesively bonded inside aluminum joints: experimental and numerical study
Carbon fiber-reinforced polymer pultrusions adhesively bonded inside aluminum joints: experimental and numerical study
A 3-D finite element model for thermal analysis of laser assisted fiber placement
A 3-D finite element model for thermal analysis of laser assisted fiber placement
Experimental assessment of the influence of welding process parameters on Lamb wave transmission across ultrasonically welded thermoplastic composite joints
Experimental assessment of the influence of welding process parameters on Lamb wave transmission across ultrasonically welded thermoplastic composite joints
The effect of temperature on fatigue crack growth in FM94 epoxy adhesive bonds investigated by means of energy dissipation
The effect of temperature on fatigue crack growth in FM94 epoxy adhesive bonds investigated by means of energy dissipation
Mode I fatigue delamination growth with fibre bridging in multidirectional composite laminates
Mode I fatigue delamination growth with fibre bridging in multidirectional composite laminates
Full-scale testing of an ultrasonic guided wave based structural health monitoring system for a thermoplastic composite aircraft primary structure
Full-scale testing of an ultrasonic guided wave based structural health monitoring system for a thermoplastic composite aircraft primary structure
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