Through-thickness thermal conduction in glass fiber polymer–matrix composites and its enhancement by composite modification

2015 ◽  
Vol 51 (7) ◽  
pp. 3463-3480 ◽  
Author(s):  
Yoshihiro Takizawa ◽  
D. D. L. Chung
Keyword(s):  
Glass Fiber ◽  
Polymer Matrix ◽  
Thermal Conduction ◽  
Polymer Matrix Composites ◽  
Matrix Composites ◽  
Composite Modification

Silane-Treated E-Glass Fiber-Reinforced Telechelic Macromer-Based Polymer-Matrix Composites

Silicon ◽  
2013 ◽  
Vol 6 (1) ◽  
pp. 57-63 ◽  
Author(s):  
Mervi Puska ◽  
Meng Zhang ◽  
Jukka P. Matinlinna ◽  
Pekka K. Vallittu
Keyword(s):  
Glass Fiber ◽  
Polymer Matrix ◽  
Polymer Matrix Composites ◽  
Matrix Composites ◽  
Fiber Reinforced ◽  
Glass Fiber Reinforced

Experimental and Numerical Validation of Unmanned Aerial Vehicle Structure Fabricated using Graphene based Polymer Matrix Composites

2021 ◽  
Vol 13 (1) ◽  
Author(s):  
R. VijayKumar ◽  
S.K. Maharana
Keyword(s):  
Glass Fiber ◽  
Polymer Matrix ◽  
Polymer Matrix Composites ◽  
Peak Load ◽  
Experimental Studies ◽  
Weight Ratio ◽  
Matrix Composites ◽  
Glass Fiber Reinforced ◽  
Layer Composite ◽  
Strength And Stiffness

This paper describes the investigation of the polymer matrix composite laminate of epoxy resin systems and graphene oxide (GO) reinforced with glass fiber. The laminates of epoxy glass fiber reinforced with GO has been fabricated by hand layup method and the fabricated laminate is further cut into test specimens as per ASTM standards and tested for their strength and stiffness. As per the experimental studies, the strength to weight ratio is increased. An attempt has also been made to observe how the different volume addition (1.5%, 3%, 4.5% and 6%) of GO to epoxy matrix has affected the tensile strength, Young’s modulus and % elongation of the laminate made of composite. The outcome of the experimental characterization of the composites has encouraged further choosing epoxy / GO (1.5% by volume) towards fabricating a simplified version of UAV. Laminate code EPWM12, an epoxy / GO woven mat 12-layer composite, has the satisfying peak load carrying capacity as well as three-point flexural strength as opposed to other four materials considered in this study. The Monte Carlo simulation showed that likelihood of EPWM12 material being safe for UAV is 96%.

scholarly journals Effect of carbon/glass fiber symmetric inter-ply sequence on mechanical properties of polymer matrix composites

2018 ◽  
Vol 20 ◽  
pp. 530-535 ◽  
Author(s):  
Dipak Kumar Jesthi ◽  
Pravanjan Mandal ◽  
Arun Kumar Rout ◽  
Ramesh Kumar Nayak
Keyword(s):  
Mechanical Properties ◽  
Glass Fiber ◽  
Polymer Matrix ◽  
Polymer Matrix Composites ◽  
Matrix Composites
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