Investigation of Charpy impact behavior of porous twisted wire material

2017 ◽  
Vol 32 (12) ◽  
pp. 2276-2285 ◽  
Author(s):  
Zhaoyao Zhou ◽  
Liuyang Duan ◽  
Fei Wu
Keyword(s):  
Charpy Impact ◽  
Impact Behavior ◽  
Wire Material ◽  
Image Position ◽  
Twisted Wire

Abstract

scholarly journals Bend and Shear Tests: Suitable Methods for Mechanical Characterization of Laminated Composite Materials

2007 ◽  
Vol 539-543 ◽  
pp. 901-906 ◽  
Author(s):  
Fernando Carreño ◽  
M. Pozuelo ◽  
José A. Jiménez ◽  
Oscar A. Ruano
Keyword(s):  
Mechanical Properties ◽  
Mechanical Characterization ◽  
Laminated Composite ◽  
Charpy Impact ◽  
Impact Behavior ◽  
Bond Quality ◽  
Shear Tests ◽  
Graphical Visualization ◽  
Laminated Composite Materials

Bend and shear tests were used to characterize the improvement in impact behavior of various ultrahigh carbon steel laminated composites. These tests turned out to deliver much more useful information about the mechanical properties of the laminates than the Charpy impact tests and were especially interesting for characterization of laminates of very high toughness values. The toughness of the various laminates was controlled by the rolling conditions that determined the quality of the bond and the appearance of delamination by the interfaces. The bend test allows determination of yield and maximum stresses, absorbed energy and permits graphical visualization of layer fracture and delaminations as testing proceeds. The shear test allows mechanical characterization of the bond quality between layers, permitting prediction of possible delaminations, and therefore, the mechanical properties of the layered material.

Experimental investigation on tensile and Charpy impact behavior of Kevlar/S-glass/epoxy hybrid composite laminates

2017 ◽  
Vol 37 (2) ◽  
pp. 177-184 ◽  
Author(s):  
Ahmet Erkliğ ◽  
Mehmet Bulut
Keyword(s):  
Impact Strength ◽  
Hybrid Composite ◽  
Composite Laminates ◽  
Glass Fibers ◽  
Impact Resistance ◽  
Charpy Impact ◽  
Side Impact ◽  
Impact Behavior ◽  
Absorbed Energy ◽  
Mixing Ratios

Abstract The aim of this study is to evaluate the effect of hybridizing Kevlar and glass fibers on the tensile and Charpy impact properties of their composites. Produced hybrid samples were designed as unbalanced and asymmetric structures in terms of different mixing ratios between woven Kevlar and S-glass fibers, and their tensile properties were determined using ASTM standards. A series of Charpy impact tests were performed to evaluate the amount of impact strength and absorbed energy by impacting each side of the hybrid composite samples. When the hybrid samples were impacted on the surface of the Kevlar side, they exhibited higher impact resistance compared with glass side impact. The resulting degree of hybridization effects showed that addition of Kevlar layers instead of glass layers contributed a significant increase in impact strength and absorbed energy of the overall composite laminate.

Impact Behavior of Cracked Plate Repaired with Composite and FML Patches

2008 ◽  
Vol 47-50 ◽  
pp. 612-616 ◽  
Author(s):  
Mehdi Sadeghinia ◽  
Seyyed Mohammad Reza Khalili ◽  
R. Ghadjar
Keyword(s):  
Crack Length ◽  
Charpy Impact ◽  
Thin Layers ◽  
Impact Behavior ◽  
Single Edge ◽  
Absorbed Energy ◽  
Cracked Plate ◽  
Cracked Plates ◽  
Single Side ◽  
The Impact

In this paper, the impact behavior of repaired cracked plates was investigated experimentally. single edge cracked aluminum plate having crack length to width ratios of 0.1, 0.3 and 0.5 was repaired with four different patch configurations namely: 3 layer GRP, 5 layer GRP patch, 2/1 FML patch and 3/2 FML patches tested in Charpy impact and the energy absorbed by specimens were compared together and compared with the unrepaired cracked plate. FML patches were made of thin layers of glass/epoxy composites of 0.2 mm thickness with phosphor bronze sheets of 0.2 mm thickness. The patching was single side. The composite and FML patching was more effective in repairing the specimens with greater crack length. Placing 3 GRP and 5 GRP patches increased the absorbed energy by only 3 to 4 joules respectively as compared to unrepaired plate. The use of 2/1 and 3/2 FML patches could increase the absorbed energy two to four times depend on crack length.

scholarly journals Effect of grain structure on Charpy impact behavior of copper

2017 ◽  
Vol 7 (1) ◽  
Author(s):  
Ningning Liang ◽  
Yonghao Zhao ◽  
Jingtao Wang ◽  
Yuntian Zhu
Keyword(s):  
Charpy Impact ◽  
Grain Structure ◽  
Impact Behavior

Anisotropic Charpy impact behavior of novel interpenetrating phase composites

Vacuum ◽  
2018 ◽  
Vol 155 ◽  
pp. 83-90 ◽  
Author(s):  
Bibo Yao ◽  
Zhaoyao Zhou ◽  
Liuyang Duan ◽  
Zengtao Chen
Keyword(s):  
Charpy Impact ◽  
Impact Behavior ◽  
Interpenetrating Phase Composites

The Charpy Impact Behavior of Fe3Al and Fe3Al-20 at % Mn Alloys

1996 ◽  
Vol 460 ◽  
Author(s):  
J. N. Liu ◽  
W. Yan ◽  
J. L. Ma ◽  
K. H. Wu
Keyword(s):  
Impact Energy ◽  
Charpy Impact ◽  
Testing Temperature ◽  
Impact Behavior ◽  
Al Alloy ◽  
Impact Fracture Behavior ◽  
Series Of Experiments ◽  
Growth Energy ◽  
The Impact ◽  
Total Impact

ABSTRACTA series of experiments were conducted to investigate the impact fracture behavior of Fe3Al and Fe3Al-20 Mn alloys. The results of this study indicated that: (i) The addition of Mn introduces an ordered Ll2-type phase in the Fe3Al-based alloys. On the other hand, the addition of Mn decreases the order parameter of the DO3 a phase, (ii) The total- impact energy of an Fe3Al alloy increases with the temperature at the low-temperature range (<600°C), then drops around 700°C, and finally increases again as the temperature further elevates, (iii) The trend of the variation of the impact energy of Fe3Al-20 at % Mn alloy with temperature is the same as that of the Fe3Al alloy, (iv) And the addition of Mn significantly improves the impact energy of the Fe3Al-based alloy, and changes the variation of the crack-growth energy with the testing temperature when the temperature is above 700°C.

Sign in / Sign up

Export Citation Format

Share Document