[HTML][HTML] Design of adhesively bonded lap joints with laminated CFRP adherends: Review, challenges and new opportunities for aerospace structures
J Kupski, ST De Freitas - Composite Structures, 2021 - Elsevier
Adhesive bonding is one of the most suitable joining technologies in terms of weight and
mechanical performance for current carbon fiber reinforced polymer aircraft fuselage …
mechanical performance for current carbon fiber reinforced polymer aircraft fuselage …
A review on design for manufacture of variable stiffness composite laminates
GG Lozano, A Tiwari, C Turner… - Proceedings of the …, 2016 - journals.sagepub.com
The use of curvilinear fibre paths to develop variable stiffness laminates is now recognised
as a promising technique offering great potential for performance improvements over …
as a promising technique offering great potential for performance improvements over …
Modelling and simulation methodology for unidirectional composite laminates in a Virtual Test Lab framework
A reliable virtual testing framework for unidirectionally laminated composites is presented
that allows the prediction of failure loads and modes of general in-plane coupons with great …
that allows the prediction of failure loads and modes of general in-plane coupons with great …
Reliability-based design optimization of laminated composite structures under delamination and material property uncertainties
Delamination is a major type of defects from manufacturing process in laminated composite
structures, exhibiting uncertain characteristics which are represented by mixed random …
structures, exhibiting uncertain characteristics which are represented by mixed random …
Gradient ply thickness design for enhanced low-velocity impact resistance in ultra-thin ply composite
The use of ultra-thin plies in composite laminates offers several advantages over traditional
plies. These include increased design flexibility, improved damage tolerance, and enhanced …
plies. These include increased design flexibility, improved damage tolerance, and enhanced …
Low‐velocity impact response and damage tolerance of hybrid biaxial/triaxial braided composite laminates
Z Wu, K Wang, L Shi, X Cheng, Y Yuan - Polymer Composites, 2023 - Wiley Online Library
The structural properties of braided composite laminates are significantly affected by the low‐
velocity impact (LVI). In this paper, the impact resistance and damage tolerance of triaxial …
velocity impact (LVI). In this paper, the impact resistance and damage tolerance of triaxial …
[HTML][HTML] Composite layup effect on the failure mechanism of single lap bonded joints
Single lap bonded joints with four different composite adherend stacking sequences were
tested and numerically simulated. The aim was to evaluate the effect of the layups on the …
tested and numerically simulated. The aim was to evaluate the effect of the layups on the …
Damage resistance and damage tolerance of dispersed CFRP laminates: Effect of the mismatch angle between plies
Damage resistance and damage tolerance to impact events is the most demanding criteria
in sizing several aeronautical composites. Tailoring the laminate ply sequence represents …
in sizing several aeronautical composites. Tailoring the laminate ply sequence represents …
[HTML][HTML] Using thin-plies to improve the damage resistance and tolerance of aeronautical CFRP composites
Thin-ply composites are currently receiving specific attention from researchers due to their
capabilities to delay matrix cracking. In this paper, the aim is to design a hybrid laminate that …
capabilities to delay matrix cracking. In this paper, the aim is to design a hybrid laminate that …
Damage resistance and damage tolerance of dispersed CFRP laminates: Effect of ply clustering
In this paper, the effect of introducing ply clustering in a composite stacking sequence on the
damage resistance and damage tolerance of CFRP composite plates is investigated. Three …
damage resistance and damage tolerance of CFRP composite plates is investigated. Three …