In this study, new efficient designs for adhesive sandwich T-joint and single-lap joint were proposed and investigated. In the proposed new sandwich T-joint, called U-channel joint, the load transfer path at the web-flange interface was modified to include a U-shaped aluminum channel which provides strong path for load transfer. Experimental results show that the new design has 62% more strength than the conventional circular fillet joint. The new U-channel joint was tested in tension, compression and bending to investigate its characteristics. It is found to have good performance in bending also, even though in compression it performs same as the circular fillet joint. An extensive parametric study was carried out to investigate the effect...
Joining by adhesively bonded methods is being increasingly used in the design of mechanical structur...
Two series of single-lap, single-bolt composite joints were tested to failure in tension. The princi...
The behaviour of various aircraft lap joint repair configurations is investigated experimentally and...
This paper presents an investigation into the failure behaviour of composite sandwich T-joint struct...
Metal and composite plates can be bonded together to form a joint known as the "single-lap" joint. T...
This paper describes progress towards developing design guidelines for a number of composite bonded ...
Composite sandwich structures are used extensively in aerospace, marine and other industrial applica...
In this study, a novel design of adhesive single-lap joint was proposed and investigated. In this ne...
Glass and carbon fiber reinforced polymer composite materials are predominantly finding wider use in...
Composite sandwich structures are widely used in many fields. T-joint plays a significant role in th...
Currently, composite joints have become vital since the structural properties of the composite struc...
Although the best configuration of the joints used to connect a common GFRP sandwich panel with the ...
This study presents an investigation into the failure mechanism and strength improvement of a sandwi...
The paper presents a comparative analysis of the strength properties of single-lap assembly joints. ...
Currently, composite joints have become vital since the structural properties of the composite struc...
Joining by adhesively bonded methods is being increasingly used in the design of mechanical structur...
Two series of single-lap, single-bolt composite joints were tested to failure in tension. The princi...
The behaviour of various aircraft lap joint repair configurations is investigated experimentally and...
This paper presents an investigation into the failure behaviour of composite sandwich T-joint struct...
Metal and composite plates can be bonded together to form a joint known as the "single-lap" joint. T...
This paper describes progress towards developing design guidelines for a number of composite bonded ...
Composite sandwich structures are used extensively in aerospace, marine and other industrial applica...
In this study, a novel design of adhesive single-lap joint was proposed and investigated. In this ne...
Glass and carbon fiber reinforced polymer composite materials are predominantly finding wider use in...
Composite sandwich structures are widely used in many fields. T-joint plays a significant role in th...
Currently, composite joints have become vital since the structural properties of the composite struc...
Although the best configuration of the joints used to connect a common GFRP sandwich panel with the ...
This study presents an investigation into the failure mechanism and strength improvement of a sandwi...
The paper presents a comparative analysis of the strength properties of single-lap assembly joints. ...
Currently, composite joints have become vital since the structural properties of the composite struc...
Joining by adhesively bonded methods is being increasingly used in the design of mechanical structur...
Two series of single-lap, single-bolt composite joints were tested to failure in tension. The princi...
The behaviour of various aircraft lap joint repair configurations is investigated experimentally and...