DocumentCode :
2682060
Title :
Residual strength assessment to panels with multiple site damage by method of system reliability
Author :
Wu, Ningxiang ; Xie, Liyang ; Zhao, Fei ; Chen, Bo
Author_Institution :
Sch. of Mech. Eng. & Autom., Northeastern Univ., Shenyang, China
fYear :
2011
fDate :
12-15 June 2011
Firstpage :
74
Lastpage :
79
Abstract :
The residual strength prediction and assessment of panels with MSD is very important to aged airplane. This paper presented the load-sharing parallel system reliability model to assess residual strength of this kind of structure. The model treated the structure as a load-sharing parallel system with different type components since different ligaments have different area. The probability distribution of the residual strength of system was derived by Monte Carlo simulation method. The model was verified by test results and most relative errors to test results for this model are about 10 percent.
Keywords :
Monte Carlo methods; aircraft; mechanical strength; reliability; statistical distributions; structural panels; Monte Carlo simulation method; aged airplane; load-sharing parallel system reliability model; multiple site damage panels; probability distribution; residual strength; residual strength assessment; Atmospheric modeling; Ligaments; Load modeling; Materials; Monte Carlo methods; Reliability; Stress; load-sharing parallell system; multiple site damage; residual stength; system reliability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability, Maintainability and Safety (ICRMS), 2011 9th International Conference on
Conference_Location :
Guiyang
Print_ISBN :
978-1-61284-667-5
Type :
conf
DOI :
10.1109/ICRMS.2011.5979236
Filename :
5979236
Link To Document :
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