Continuous variation of stiffness across flat plates has been shown, theoretically, to improve buckling performance by up to 60%. However, steered fibre manufacturing methods cannot achieve the minimum radius of curvature required for improvement whilst maintaining a high deposition rate. An alternative concept, Discrete Stiffness Tailoring (DST), which varies stiffness within a ply through discrete changes of angle, is compatible with high rate deposition methods such as Advanced Tape Laying. Through the simple example of redistribution of the material in a quasi-isotropic [±45/90/0]2S laminate whilst maintaining ply percentages, DST is shown both experimentally and theoretically to improve buckling stress by at least 15% with no indicatio...
The use of composite materials in airplanes has been increasing over the last decades, mainly due to...
Double angle-ply or ‘Double-Double’ (DD) laminates offer new design possibilities in laminated compo...
Significant improvements in the mechanical performance of a laminated composite structure can be ach...
Continuous variation of stiffness across flat plates has been shown, theoretically, to improve buckl...
Discrete Stiffness Tailoring (DST) is a novel manufacturing concept where stiffness tailoring is ach...
This article presents an algorithm to tailor bending stiffness properties for double angle-ply lamin...
peer-reviewedComposite materials are finding increasing application, for example in commercial aircr...
Over the past decades, fibre-reinforced composite structures have been increasingly adopted into mai...
A novel low-cost manufacturing process is introduced, referred to as ‘Fabric Steering’. By manipulat...
Tailoring composite laminates to vary the fiber orientations within a fiber layer of a laminate to a...
Engineers are still looking for ways to improve the performance of materials used in aircraft. A maj...
A novel form of fiber steering (Continuous TowShearing (CTS)) which eliminates manufacturingdefects ...
Automated fibre placement technology has made possible to place bands of composite fibre tows along ...
This data item provides supplementary information to an article entitled: Laminate Stiffness Tailori...
Variable Angle Tow designs have shown to improve structural performance by providing a better stiffn...
The use of composite materials in airplanes has been increasing over the last decades, mainly due to...
Double angle-ply or ‘Double-Double’ (DD) laminates offer new design possibilities in laminated compo...
Significant improvements in the mechanical performance of a laminated composite structure can be ach...
Continuous variation of stiffness across flat plates has been shown, theoretically, to improve buckl...
Discrete Stiffness Tailoring (DST) is a novel manufacturing concept where stiffness tailoring is ach...
This article presents an algorithm to tailor bending stiffness properties for double angle-ply lamin...
peer-reviewedComposite materials are finding increasing application, for example in commercial aircr...
Over the past decades, fibre-reinforced composite structures have been increasingly adopted into mai...
A novel low-cost manufacturing process is introduced, referred to as ‘Fabric Steering’. By manipulat...
Tailoring composite laminates to vary the fiber orientations within a fiber layer of a laminate to a...
Engineers are still looking for ways to improve the performance of materials used in aircraft. A maj...
A novel form of fiber steering (Continuous TowShearing (CTS)) which eliminates manufacturingdefects ...
Automated fibre placement technology has made possible to place bands of composite fibre tows along ...
This data item provides supplementary information to an article entitled: Laminate Stiffness Tailori...
Variable Angle Tow designs have shown to improve structural performance by providing a better stiffn...
The use of composite materials in airplanes has been increasing over the last decades, mainly due to...
Double angle-ply or ‘Double-Double’ (DD) laminates offer new design possibilities in laminated compo...
Significant improvements in the mechanical performance of a laminated composite structure can be ach...