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.
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 :
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