Results 51 to 60 of about 2,040,887 (358)
Discrete ply model of circular pull-through test of fasteners in laminates [PDF]
, 2012 In aeronautical structures, assemblies with thin laminates are becoming increasingly usual, especially for fuselage design. In these structures, out-of-plane loads can appear in bolted joints and can lead to progressive punching of the fastener’s head in
Bouvet, Christophe +4 more
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Composites Part C: Open Access, 2021 A methodology is proposed to incorporate spatial distributions of micro-defects within a three dimensional multiscale modeling framework for Carbon Fiber Reinforced Polymer (CFRP) composites to predict stiffness and strength properties of laminates for ...
Rudraprasad Bhattacharyya, Douglas Adams
doaj +1 more source
Delamination of Z-pinned carbon fibre reinforced laminates [PDF]
, 2005 The paper outlines the current status of mechanical testing, identification of failure mechanisms and data analysis related to delamination cracking in high performance laminates made via the prepreg/autoclave route, strengthened in the through ...
Cartié, Denis D. R. +2 more
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FEBS Letters, EarlyView.Drosophila park mutants serve as a model for Parkinson's disease. We used this strain to investigate the connection between oxidative stress and the circadian clock mechanism. We showed that increased oxidative stress affects the physiology of pacemaker cells, disrupting their daily structural plasticity. Lack of rhythmic signaling from pacemaker cells
Kamila Zientara +3 more
wiley +1 more source
Fatigue crack growth in thin notched woven glass composites under tensile loading. Part I: experimental [PDF]
, 2011 Helicopter blades are made of composite materials mainly loaded in fatigue and have normally relatively thin skins. A through-the-thickness crack could appear in these skins.
Barrau, Jean-Jacques +7 more
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International Journal of Lightweight Materials and ManufactureNumerous studies have investigated the advantages of using composite laminates made of both metals and fibers, which include being able to sustain heavier loads, having better resistance to impacts, and being more durable, while also being lightweight ...
Benediktus Madika, Anne Z. Syahrial
doaj +1 more source
SPH-FEM Design of Laminated Plies under Bird-Strike Impact
Aerospace, 2019 Composite laminates can potentially reduce the weight of aircrafts; however, they are subjected to bird strike hazards in civil aviation. To handle their nonlinear dynamic behaviour, in this study, the impact damage of composite laminates were ...
Yadong Zhou, Youchao Sun, Tianlin Huang
doaj +1 more source
The strength recovery effect of scarf bonding on the CFRP laminates with impact damage
Heliyon, 2023 Impact damage can affect the carrying capacity and service life of aerospace composite structures seriously. In this study, the carbon fiber/epoxy composite (ZT7H/EC3448) was used for scarf bonding repair for CFRP (Z7TH/QY9611) laminates to restore ...
Xue Xiao, Xuan Shanyong, Fu Bin
doaj +1 more source
Molecular Oncology, EarlyView.Dimethyl fumarate (DMF) reduces growth of HPV‐positive cervical cancer spheroids and induces ferroptosis in cervical cancer cells via blocking SLC7A11/Glutathione (GSH) axis. Combination of subcytotoxic doses of DMF and cisplatin (CDDP) further suppresses spheroid growth and drives cell death in 2D culture models.
Carolina Punziano +6 more
wiley +1 more source
The Effects of fibre pre-stressing on the impact performance of composite laminates [PDF]
, 2011 This thesis has presented the results and findings of a study carried out into the effects of fibre pre-stressing on the impact performance of composite laminates.
Jevons, Matthew Paul
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