Manufacturable insight into modelling and design considerations in fibre-steered composite laminates: State of the art and perspective
The advent of novel robot-assisted composite manufacturing techniques has enabled
steering of fibre paths in the plane of the lamina, leading to the emergence of the so-called …
steering of fibre paths in the plane of the lamina, leading to the emergence of the so-called …
Recent developments in manufacturing, mechanics, and design optimization of variable stiffness composites
D Punera, P Mukherjee - Journal of Reinforced Plastics and …, 2022 - journals.sagepub.com
The functional advantages of tailored stiffness, often seen in nature, are also utilized in
composite structures. Advancements in the multiaxis tow placement and automated fiber …
composite structures. Advancements in the multiaxis tow placement and automated fiber …
Geometrically nonlinear dynamic analysis of variable stiffness composite laminated and sandwich shell panels
A Gupta, S Pradyumna - Thin-Walled Structures, 2022 - Elsevier
The nonlinear free and forced vibration analyses of variable stiffness composite laminated
(VSCL) and sandwich shell panels having curvilinear fibres, not yet reported in literature, are …
(VSCL) and sandwich shell panels having curvilinear fibres, not yet reported in literature, are …
[HTML][HTML] Assessment of layerwise user-elements in Abaqus for static and free vibration analysis of variable stiffness composite laminates
In this work, user-elements (UEL) in Abaqus are taken a step forward into the high-order
layerwise modelling of variable stiffness composite laminates with curvilinear fibre paths …
layerwise modelling of variable stiffness composite laminates with curvilinear fibre paths …
Higher-order structural theories for the static analysis of doubly-curved laminated composite panels reinforced by curvilinear fibers
The main aim of this paper is the evaluation of the through-the-thickness profiles of strain,
stress and displacement components of several doubly-curved panels reinforced by …
stress and displacement components of several doubly-curved panels reinforced by …
Geometrically nonlinear bending analysis of variable stiffness composite laminated shell panels with a higher-order theory
A Gupta, S Pradyumna - Composite Structures, 2021 - Elsevier
A finite element (FE) formulation is developed by extending the third-order shear
deformation theory, including the zig-zag effects using the Murakami zig-zag function, for the …
deformation theory, including the zig-zag effects using the Murakami zig-zag function, for the …
[HTML][HTML] Analysis of variable angle tow composites structures using variable kinematic models
This work presents a refined beam model based on the Carrera Unified Formulation for the
free-vibration analyses of variable stiffness composite laminate characterized by layers with …
free-vibration analyses of variable stiffness composite laminate characterized by layers with …
Foam core composite sandwich plates and shells with variable stiffness: Effect of the curvilinear fiber path on the modal response
F Tornabene, N Fantuzzi… - Journal of Sandwich …, 2019 - journals.sagepub.com
This paper presents the free vibration analysis of composite sandwich plates and doubly
curved shells with variable stiffness. The reinforcing fibers are located in the external skins of …
curved shells with variable stiffness. The reinforcing fibers are located in the external skins of …
Equivalent single layer, zig-zag, and layer wise theories for variable angle tow composites based on the generalized unified formulation
L Demasi, G Biagini, F Vannucci, E Santarpia… - Composite …, 2017 - Elsevier
Abstract Variable Angle Tow (VAT) composites remove the constraint of having straight
fibers, typical of traditional composite structures. This dramatically increases the design …
fibers, typical of traditional composite structures. This dramatically increases the design …
Aeroelasticity of composite plates with curvilinear fibres in supersonic flow
The target of this investigation is to understand the aeroelastic (dynamic or static) instability
of variable stiffness composite laminates (VSCLs) in the presence of supersonic airflow. The …
of variable stiffness composite laminates (VSCLs) in the presence of supersonic airflow. The …