1998
DOI: 10.1023/a:1004351606897
|View full text |Cite
|
Sign up to set email alerts
|

Untitled

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
30
0

Year Published

2008
2008
2023
2023

Publication Types

Select...
5
4

Relationship

0
9

Authors

Journals

citations
Cited by 131 publications
(32 citation statements)
references
References 57 publications
0
30
0
Order By: Relevance
“…Typical microscopic damage around a fiber break in SFC includes transverse matrix cracks and/or interfacial debonding between the fiber and matrix initiated from fiber breaks [4] (Fig. 1(a)).…”
Section: Single-fiber Composite Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…Typical microscopic damage around a fiber break in SFC includes transverse matrix cracks and/or interfacial debonding between the fiber and matrix initiated from fiber breaks [4] (Fig. 1(a)).…”
Section: Single-fiber Composite Modelmentioning
confidence: 99%
“…In particular, the single-fiber composite (SFC) test has been used as a powerful tool to characterize the damage process at the constituent level (i.e. fiber, matrix, and the interface) [1][2][3][4][5][6]. In the SFC, a single-fiber embedded in the matrix suffers multiple fiber breaks (i.e.…”
Section: Introductionmentioning
confidence: 99%
“…By recording the overall strain and load on the fiber at saturation, as well as the number of breaks (current practice) and associated fragment lengths, an approximate calculation for the IFSS is obtained using models derived from the 'fiber' free body diagram shown in Figure 1. The limitations of the various micromechanical models developed to calculate the IFSS have been well documented [12][13][14][15][16][17][18][19][20][21][22]. The equation for calculating the IFSS, ߬ , has the following general form:…”
Section: Introductionmentioning
confidence: 99%
“…Stress-strain curves of EOC/short fiber composite as a function of fiber loading and length from matrix to the fiber will build up sufficient tensile stress in the fiber to its tensile strength leading to fiber fracture. Furthermore, the high length fibers may undergo entanglement with each other causing aggregate lumps of fibers which act as stress concentrated points, as a result the stressed composite leads to a low strain failure or brittle failure [26][27][28]. The stress-strain behavior and the corresponding tensile properties such as tensile strength, elongation at break, Young's modulus, low strain modulus (10%) and high strain modulus (100% ) as a function of short fiber length and loading are displayed in Figure 2 and Table 5 respectively.…”
Section: Mechanical Properties Of the Composites (A) Effect Of Short mentioning
confidence: 99%