Influence of the Manufacturing Process on the Tensile Stress-Strain Response of Hybrid Glass/Carbon and Carbon/Carbon Composites

2021 ◽  
pp. 2423-2434
Author(s):  
Zahir Namourah ◽  
Filipe Ribeiro ◽  
José Sena-Cruz
Keyword(s):  
Tensile Stress ◽  
Manufacturing Process ◽  
Carbon Composites ◽  
Strain Response ◽  
Stress Strain ◽  
Glass Carbon

scholarly journals Uniaxial Tensile Stress-Strain Response on the 3D Angle Interlock Woven Fabric Composite

2019 ◽  
Vol 7 (4.14) ◽  
pp. 430
Author(s):  
F. M.Z. Nasrun ◽  
M. F. Yahya ◽  
M. R. Ahmad ◽  
S. A. Ghani
Keyword(s):  
Tensile Stress ◽  
The Other ◽  
Woven Fabric ◽  
Uniaxial Tensile ◽  
Strain Response ◽  
Woven Composite ◽  
Stress Strain ◽  
Fabric Composite ◽  
Uniaxial Tensile Stress ◽  
Set Up

An experimental study have been performed to investigate the uniaxial tensile stress-strain response on the 3D angle interlock (3DAI) woven fabric composite. The tensile analysis were examined based on different woven fabric set-up parameter of draw-in plan ; pointed (DRW 1), broken (DRW 2), broken mirror (DRW 3), and straight (DRW 4). Meanwhile, the woven fabric composite were produced based on 22 and 25 pick.cm-1 of weft densities. The outcomes produced shown that woven composite sample with 25 pick.cm-1 on DRW 4 projected the highest stress response, 113 MPa. Extensive review indicated that DRW 1 and 4 gave better tensile stress-strain response than the other counterpart. 

First Principles Study on the TiN/BN/TiN Interface

2011 ◽  
Vol 110-116 ◽  
pp. 1020-1023 ◽  
Author(s):  
Bao Jun Wang ◽  
Fei Xie ◽  
Ke Jun Jia
Keyword(s):  
Tensile Strength ◽  
Tensile Stress ◽  
First Principles ◽  
Calculation Method ◽  
First Principles Calculation ◽  
Strain Response ◽  
Ideal Strength ◽  
Stress Strain ◽  
Electronic Density ◽  
Friedel Oscillations

To obtain a understanding of the deform mechanism and ideal strength in superhard nanocomposites nc-TiN/a-BN. we studied, using the first-principles calculation method, the geometrical stucture, the electronic density and the tensile stress-strain response of a theoretical interfacial system TiN/BN/TiN, which consists of two TiN slabs and one sandwiched BN monolayer. The calculated results show that Friedel oscillations weaken the Ti-N interplanar bonds next to the interface, where decohesion happens. A comparison with the TiN/SiN/TiN interface was done, showing that the orientation has the huger influence on the tensile strength of TiN/BN/TiN interface.

Modeling Damage Evolution in a Hybrid Ceramic Matrix Composite Under Static Tensile Load

1997 ◽  
Vol 119 (4) ◽  
pp. 401-407 ◽  
Author(s):  
N. Bonora ◽  
G. Newaz
Keyword(s):  
Tensile Stress ◽  
Damage Evolution ◽  
Failure Modes ◽  
Strain Response ◽  
Load Drop ◽  
Stress Strain ◽  
Matrix Cracks ◽  
The Matrix ◽  
Constitutive Response ◽  
Hybrid Ceramic

In this investigation, damage evolution in a unidirectional hybrid ceramic composite made from Nicalon and SiC fibers in a Lithium Aluminosilicate (LAS) glass matrix was studied. The static stress-strain response of the composite exhibited a linear response followed by load drop in a progressive manner. Careful experiments were conducted stopping the tests at various strain levels and using replication technique, scanning and optical microscopy to monitor the evolution of damage in these composites. It was observed that the constituents of the composite failed in a sequential manner at increasing strain levels. The matrix cracks were followed by SiC fiber failures near ultimate tensile stress. After that, the load drop was associated with progressive failure of the Nicalon fibers. Identification of these failure modes were critical to the development of a concentric cylinder model representing all three constituent phases to predict the constitutive response of the CMC computationally. The strain-to-failure of the matrix and fibers were used to progressively fail the constituents in the model and the overall experimental constitutive response of the CMC was recovered. A strain based analytical representation was developed relating stiffness loss to applied strain. Based on this formulation, damage evolution and its consequence on tensile stress-strain response was predicted for room temperature behavior of hybrid CMCs. The contribution of the current work is that the proposed strain-damage phenomenological model can capture the damage evolution and the corresponding material response for continuous fiber-reinforced CMCs. The modeling approach shows much promise for the complex damage processes observed in hybrid CMCs.

Unidirectional Tensile Stress-Strain Response of BP-SiC Fiber Reinforced Ti-6Al-4V

1994 ◽  
Vol 16 (3) ◽  
pp. 225 ◽  
Author(s):  
WS Johnson ◽  
JE Masters ◽  
T Kevin O'Brien ◽  
DS Li ◽  
MR Wisnom
Keyword(s):  
Tensile Stress ◽  
Strain Response ◽  
Fiber Reinforced ◽  
Stress Strain ◽  
Sic Fiber

Experimental Characterization of Mechanical Behavior of Cord-Rubber Composites

1982 ◽  
Vol 10 (1) ◽  
pp. 37-54 ◽  
Author(s):  
M. Kumar ◽  
C. W. Bert
Keyword(s):  
Response Characteristic ◽  
Cord Compression ◽  
Complete Characterization ◽  
Strain Response ◽  
Strain Gages ◽  
Experimental Characterization ◽  
Rubber Composites ◽  
Stress Strain ◽  
Strain Data

Abstract Unidirectional cord-rubber specimens in the form of tensile coupons and sandwich beams were used. Using specimens with the cords oriented at 0°, 45°, and 90° to the loading direction and appropriate data reduction, we were able to obtain complete characterization for the in-plane stress-strain response of single-ply, unidirectional cord-rubber composites. All strains were measured by means of liquid mercury strain gages, for which the nonlinear strain response characteristic was obtained by calibration. Stress-strain data were obtained for the cases of both cord tension and cord compression. Materials investigated were aramid-rubber, polyester-rubber, and steel-rubber.

Sign in / Sign up

Export Citation Format

Share Document