Recent Advances in Fracture Mechanics 1998
DOI: 10.1007/978-94-017-2854-6_17
|View full text |Cite
|
Sign up to set email alerts
|

Predicting crack initiation in composite material systems due to a thermal expansion mismatch

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
6
0

Year Published

2002
2002
2019
2019

Publication Types

Select...
5
1

Relationship

0
6

Authors

Journals

citations
Cited by 7 publications
(6 citation statements)
references
References 4 publications
0
6
0
Order By: Relevance
“…However, some of the thermal stress could not be alleviated. In this case, residual stress forms at the SiC particle layer/filler metal interface, causing the failure of the joint under external loads [19], as shown in Figures 8(a) and 8(c). According to the analysis software measurement results, SiC volume fraction in the SiC particle layer increases as SiC concentration increases from 3 g/m 2 to 16 g/m 2 .…”
Section: Mechanical Properties Of the Jointsmentioning
confidence: 99%
“…However, some of the thermal stress could not be alleviated. In this case, residual stress forms at the SiC particle layer/filler metal interface, causing the failure of the joint under external loads [19], as shown in Figures 8(a) and 8(c). According to the analysis software measurement results, SiC volume fraction in the SiC particle layer increases as SiC concentration increases from 3 g/m 2 to 16 g/m 2 .…”
Section: Mechanical Properties Of the Jointsmentioning
confidence: 99%
“…Modelling of such stresses has thus been achieved for unidirectional fibre-reinforced composites of infinite length and two-dimensional solutions (generalized plane strain) can be found in the works of Mikata and Taya [3] and Anifantis et al [4]. For a finite specimen length, close-form solutions based on a more general three-dimensional approach have recently been derived by Folias et al [5] and Quek [6]. For the single fibre push-out problem, Chai and Mai [7] proposed a model of stress transfer by considering interface roughness and thermal residual stresses.…”
Section: Introductionmentioning
confidence: 97%
“…Residual stresses can have intense effects on the mechanical properties of a composite product, such as compressive and buckling strength, fracture toughness, and fatigue strength, since a ''pre-loading'' has been introduced [2]. They also have a major effect on the micro-stresses within a composite material system and must be added to the stresses induced by the external mechanical loads [3,4]. This goes against the current trend in aerospace and other industries to develop large integrated structures to reduce the expensive cost of assembling small parts.…”
Section: Introductionmentioning
confidence: 99%