DocumentCode
3438354
Title
Notice of Retraction
Effect of accelerated ageing on the mechanical properties of composite repaired aluminum plates
Author
Zun Wang ; Yishan Zhang ; Jun Xue ; Wei Yang
Author_Institution
Beijing Aeronaut. Technol. Res. Center, Beijing, China
fYear
2013
fDate
15-18 July 2013
Firstpage
863
Lastpage
866
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Center-cracked aluminum plates were repaired with single-sided composite patches. The effects of accelerated ageing test on the static and fatigue properties of the specimens were studied. The results show that its mechanical properties are slightly affected by the accelerated one-cycle ageing test. The static bearing capability of the aged specimen is lowered by 2.5%. The fatigue lives of the repaired and aged specimens increased by 8.2 and 8.8 times, respectively, as compared with that of the unrepaired ones.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Center-cracked aluminum plates were repaired with single-sided composite patches. The effects of accelerated ageing test on the static and fatigue properties of the specimens were studied. The results show that its mechanical properties are slightly affected by the accelerated one-cycle ageing test. The static bearing capability of the aged specimen is lowered by 2.5%. The fatigue lives of the repaired and aged specimens increased by 8.2 and 8.8 times, respectively, as compared with that of the unrepaired ones.
Keywords
ageing; composite materials; cracks; plates (structures); accelerated ageing test; center cracked aluminum plates; composite repaired aluminum plates; one cycle ageing test; single sided composite patches; static bearing capability; Accelerated aging; Aircraft; Aluminum; Fatigue; Life estimation; Maintenance engineering; bonded repair; composite patch; crack; fatigue; static;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4799-1014-4
Type
conf
DOI
10.1109/QR2MSE.2013.6625705
Filename
6625705
Link To Document