Experimental Investigation on Tensile Properties of Carbon Fabric-Glass Fabric-Kevlar Fabric-Epoxy Hybrid Composite Laminates

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F21%3APU144256" target="_blank" >RIV/00216305:26210/21:PU144256 - isvavai.cz</a>

Výsledek na webu

<a href="https://www.scopus.com/record/display.uri?eid=2-s2.0-85110048966&origin=resultslist&sort=plf-f&src=s&st1=Experimental+Investigation+on+Tensile+Properties+of+Carbon+Fabric-Glass+Fabric-Kevlar+Fabric-Epoxy+Hybrid+Composite+Laminates&sid=3455efad6e6bfdbdd2d" target="_blank" >https://www.scopus.com/record/display.uri?eid=2-s2.0-85110048966&origin=resultslist&sort=plf-f&src=s&st1=Experimental+Investigation+on+Tensile+Properties+of+Carbon+Fabric-Glass+Fabric-Kevlar+Fabric-Epoxy+Hybrid+Composite+Laminates&sid=3455efad6e6bfdbdd2d</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.18280/rcma.310305" target="_blank" >10.18280/rcma.310305</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Experimental Investigation on Tensile Properties of Carbon Fabric-Glass Fabric-Kevlar Fabric-Epoxy Hybrid Composite Laminates

Popis výsledku v původním jazyce

In this paper, composite and hybrid composite materials were prepared using the hand lay-up method, with carbon, glass, and Kevlar fabrics as the reinforcing materials and epoxy as a matrix. The tensile test was performed to determine the optimal ratio of epoxy resin in carbon fabric/epoxy, glass fabric/epoxy, and Kevlar fabric/epoxy composites in terms of tensile properties. It was found that the optimal ratio of epoxy in terms of tensile properties to impregnate the used Kevlar fabric, glass fabric, and carbon fabric was around 45%wt, 3%wt, and 30%wt, respectively. The effect of fabric content and stacking sequences, with a fixed epoxy content, on the hybrid composites' tensile properties were also investigated. The tensile properties of the prepared composites were compared to determine the most favorable preparation conditions for obtaining a hybrid laminate that has high tensile properties and is suitable for a wide range of applications at a low cost.

Název v anglickém jazyce

Experimental Investigation on Tensile Properties of Carbon Fabric-Glass Fabric-Kevlar Fabric-Epoxy Hybrid Composite Laminates

Popis výsledku anglicky

In this paper, composite and hybrid composite materials were prepared using the hand lay-up method, with carbon, glass, and Kevlar fabrics as the reinforcing materials and epoxy as a matrix. The tensile test was performed to determine the optimal ratio of epoxy resin in carbon fabric/epoxy, glass fabric/epoxy, and Kevlar fabric/epoxy composites in terms of tensile properties. It was found that the optimal ratio of epoxy in terms of tensile properties to impregnate the used Kevlar fabric, glass fabric, and carbon fabric was around 45%wt, 3%wt, and 30%wt, respectively. The effect of fabric content and stacking sequences, with a fixed epoxy content, on the hybrid composites' tensile properties were also investigated. The tensile properties of the prepared composites were compared to determine the most favorable preparation conditions for obtaining a hybrid laminate that has high tensile properties and is suitable for a wide range of applications at a low cost.

Druh

J_imp - Článek v periodiku v databázi Web of Science

CEP obor

—

OECD FORD obor

20505 - Composites (including laminates, reinforced plastics, cermets, combined natural and synthetic fibre fabrics; filled composites)

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2021

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Revue des Composites et des Materiaux Avances

ISSN

1169-7954

e-ISSN

—

Svazek periodika

31

Číslo periodika v rámci svazku

3

Stát vydavatele periodika

CA - Kanada

Počet stran výsledku

7

Strana od-do

145-151

Kód UT WoS článku

000672648400005

EID výsledku v databázi Scopus

2-s2.0-85110048966