DocumentCode
3435208
Title
Notice of Retraction
Failure mode effect analysis and optimal design of the wing structure
Author
Jun-Hao Guo ; Wei-Min Cui ; Feng-Zhu Zheng ; Hong-Juan Li
Author_Institution
Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´an, China
fYear
2013
fDate
15-18 July 2013
Firstpage
130
Lastpage
133
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.
The reliability of wing structure plays an important role in the safety of a plane. Under external loads, there may be some failures in the wing structure, including flaw, crack, wearing and so on. It is essential to make FMEA (failure mode effect analysis) for the wing structure to find and deal with the failures. In order to give some advice on optimal design of the wing structure, it is necessary to know the stress distribution of each component and make a finite element analysis to the structural strength. Therefore, this paper presents FMEA method and some advice on optimal design for the wing structure.
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.
The reliability of wing structure plays an important role in the safety of a plane. Under external loads, there may be some failures in the wing structure, including flaw, crack, wearing and so on. It is essential to make FMEA (failure mode effect analysis) for the wing structure to find and deal with the failures. In order to give some advice on optimal design of the wing structure, it is necessary to know the stress distribution of each component and make a finite element analysis to the structural strength. Therefore, this paper presents FMEA method and some advice on optimal design for the wing structure.
Keywords
aerospace components; air safety; cracks; design engineering; failure (mechanical); finite element analysis; mechanical strength; optimisation; reliability; stress analysis; wear; FMEA method; crack; external loads; failure mode effect analysis; finite element analysis; flaw; optimal wing structure design; plane safety; stress distribution; structural strength; wearing; wing structure failures; wing structure reliability; Educational institutions; Finite element analysis; Joints; Presses; Reliability; Skin; Stress; FMEA; finite element analysis; optimal design; wing structure;
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.2013.6625551
Filename
6625551
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