2007
DOI: 10.1016/j.ijadhadh.2006.01.011
|View full text |Cite
|
Sign up to set email alerts
|

Effect of thermal expansion coefficient on the stress distribution in solar panel

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
8
0

Year Published

2007
2007
2018
2018

Publication Types

Select...
9

Relationship

0
9

Authors

Journals

citations
Cited by 25 publications
(8 citation statements)
references
References 10 publications
(11 reference statements)
0
8
0
Order By: Relevance
“…This concept gives a better performance to the bonded structure made with dissimilar adherents. The stress dispersion and the effect of CTE on the stress of multilayers structure of the solar panel under the temperature field using analytic method is investigated in the work of Wang [22]. An elastic analysis formula for bonded joints was developed by Romilly and Clark [23] to include the composite deformation mechanisms and the thermal residual strains that arise in hybrid metalcomposite joints.…”
Section: Introductionmentioning
confidence: 99%
“…This concept gives a better performance to the bonded structure made with dissimilar adherents. The stress dispersion and the effect of CTE on the stress of multilayers structure of the solar panel under the temperature field using analytic method is investigated in the work of Wang [22]. An elastic analysis formula for bonded joints was developed by Romilly and Clark [23] to include the composite deformation mechanisms and the thermal residual strains that arise in hybrid metalcomposite joints.…”
Section: Introductionmentioning
confidence: 99%
“…While that of modified C/C samples after thermal cycling between 1773 K and room temperature in air for 20 times can be characterized by a sloping and straight line, by reason that the oxidation process of C/C matrix is mainly controlled by the rate of O 2− reaction with C/C matrix [15]. Although modification by SiC-MoSi 2 -CrSi 2 multiphase coating could improve the thermal shock resistance of C/C samples, the existence of edges and corners on the surface of C/C samples would cause the stress concentration at the tip of these edges and corners due to the mismatch of thermal expansion coefficients between the coating (˛M oSi2 = 8.1 × 10 −6 K −1 , CrSi2 = 10.5 × 10 −6 K −1 , ˛S i = 2.6 × 10 −6 K −1 , ˛S iC = 4.5 × 10 −6 K −1 ,) and C/C composites (˛C /C = 1.0 × 10 −6 K −1 ) during thermal cycling [16][17][18]. Finally, large numbers of defects were formed in the coating, which led to the linear increasing of the weight loss.…”
Section: Resultsmentioning
confidence: 99%
“…The phase velocity, c, of the incident waves is taken as c = 800 m/s. The material constants are mainly from [34][35][36] and listed in Table 1. Figure 2 shows the localization factors and dispersion curves in the first Brillouin zone for the perfect threecomponent phononic crystals when the incident angle θ 0 = 10 • .…”
Section: Numerical Examples and Discussionmentioning
confidence: 99%