DocumentCode
533543
Title
Notice of Retraction
A kind of evaluation algorithm based on the comprehensive method for fatigue cracks fuzzy
Author
Gao Qing-ji ; Jing Ming-lan
Author_Institution
Dept. of Aeronatical Autom., Civil Aviation Univ. of China, Tianjin, China
Volume
1
fYear
2010
fDate
1-2 Aug. 2010
Firstpage
421
Lastpage
424
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.
Assessment algorithm about fatigue cracks which take cracks in aircraft skin for example is studied in this paper. A fuzzy comprehensive evaluation method is proposed that can make a assessment of aircraft skin cracks objectively and accurately. The analytic hierarchy method is used to making weight distribution to various factors that affect the degree of aircraft cracks injury, finally define the Evaluation Matrix to make fuzzy comprehensive evaluation to obtain the level of severity of cracks injury. The effectiveness of the method is shown through experiments.
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.
Assessment algorithm about fatigue cracks which take cracks in aircraft skin for example is studied in this paper. A fuzzy comprehensive evaluation method is proposed that can make a assessment of aircraft skin cracks objectively and accurately. The analytic hierarchy method is used to making weight distribution to various factors that affect the degree of aircraft cracks injury, finally define the Evaluation Matrix to make fuzzy comprehensive evaluation to obtain the level of severity of cracks injury. The effectiveness of the method is shown through experiments.
Keywords
aerospace components; aircraft; decision making; fatigue cracks; fuzzy set theory; matrix algebra; aircraft skin fatigue crack; analytic hierarchy method; assessment algorithm; evaluation matrix; fuzzy comprehensive method; weight distribution; Injuries; Skin; Fuzzy Comprehensive Evaluation Method; Hierarchical clustering; The Analytic Hierarchy Process (AHP);
fLanguage
English
Publisher
ieee
Conference_Titel
Circuits,Communications and System (PACCS), 2010 Second Pacific-Asia Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4244-7969-6
Type
conf
DOI
10.1109/PACCS.2010.5626599
Filename
5626599
Link To Document