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Determination of Fatigue Limit of Coir/CNT/Fly Ash Reinforced Epoxy Polymer Matrix Composite

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TLDR
In this article, an attempt is made to reinforce green/recyclable/reusable materials in the polymer composite by making composite specimens with epoxy as matrix and coir/CNT/fly ash as reinforcements.
Abstract
In the quest of new material development, polymer matrix composite plays prominent role. Instead of reinforcing synthetic material in the polymer composite, an attempt is made in this work to reinforce green/recyclable/reusable materials in the polymer composite. Composite specimens are made with epoxy as matrix and coir/CNT/fly ash as reinforcements. The influences of wt.% of coir/CNT/fly ash on fatigue behavior of composite are determined. Response Surface Methodology (RSM), a Design of Experiments (DOE) approach is followed in specimen preparation and testing. ANOVA is used to find the influences of different parameters such as wt.% of coir/CNT/fly ash on fatigue behavior of composite. Optimized levels of parameters are also found out.

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Journal ArticleDOI

Ground tire rubber filled low-density polyethylene: The effect of particle size

TL;DR: In this article, the authors investigated the possibility of value-added recycling of ultrafine ground tire rubber (uGTR) produced from water jet milling, with an average particle size of a few tens of microns.
Journal ArticleDOI

Ground tire rubber filled low-density polyethylene: The effect of particle size

TL;DR: In this article , the authors investigated the possibility of value-added recycling of ultrafine ground tire rubber (uGTR) produced from water jet milling, with an average particle size of a few tens of microns.

Experimental Investigation on Tensile and Damping Properties of SiC and Flyash Reinforced Glass Fiber Epoxy Composites

TL;DR: In this paper, the SiC and fly ash powder is mixed as fillers with epoxy resins to characterize the mechanical and damping properties of GFRE composites, and the free vibration behavior of these specimens are observed experimentally by Universal Testing Machine (UTM).
Journal ArticleDOI

Virtual fatigue analysis of epoxy based composite reinforced with sugarcane fibre, fly ash and carbon nano tubes

TL;DR: In this article , Fatigue analysis of materials prepared using different wt.% of sugarcane, carbon nano tubes, fly-ash and carbon nano tube was carried out using ANSYS.
References
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Journal ArticleDOI

Mechanical and dynamic properties of coconut fibre reinforced concrete

TL;DR: In this article, a comparison between the static and dynamic moduli of CFRC beams was conducted, and it was found that CFRC with a fibre length of 5 cm and a fibre content of 5% has the best properties.
Journal ArticleDOI

Mechanical and thermal characteristics of high density polyethylene-fly ash Cenospheres composites

TL;DR: In this article, fly ash Cenospheres are used as reinforcing filler in High density polyethylene (HDPE) to develop lightweight composites and the tensile and thermal properties of the composites were measured according to ASTM methods.
Book ChapterDOI

Fatigue and Fracture

TL;DR: In this article, the suitability and uncertainty of physical models were considered for crack initiation and growth under cyclic loading as well as unstable crack propagation and tearing in ship and offshore structures and due attention was paid to practical application and statistical description of fracture control methods in design, fabrication and service.
Journal ArticleDOI

Enhancement of mechanical performance of epoxy/carbon fiber laminate composites using single-walled carbon nanotubes

TL;DR: In this article, single-walled carbon nanotubes (SWCNT) were used to develop nano-modified carbon fiber/epoxy laminates to improve dispersion and epoxy resin-nanotube interaction.
Journal ArticleDOI

Mechanical properties of CFRP laminates manufactured from unidirectional prepregs using CSCNT-dispersed epoxy

TL;DR: In this article, the experimental results of the mechanical properties of three-phase CFRP laminates consisting of traditional carbon fibers and epoxy matrix modified using cup-stacked carbon nanotubes (CSCNTs) in comparison to those of CFRP without CSCNT are presented.
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