An integrated fuzzy-genetic failure mode and effect analysis for aircraft wing reliability

Author:

Gholizadeh Hadi,Javadian Nikbakhsh,Fazlollahtabar Hamed

Publisher

Springer Science and Business Media LLC

Subject

Geometry and Topology,Theoretical Computer Science,Software

Reference30 articles.

1. ARP 926 (1967) Design analysis procedures for failure modes, effects and criticality analysis (FMECA). Aerospace Recommended Practice, Society of Automotive Engineers, Detroit, USA

2. Belu Nadia, Ionescu Laurenţiu (2014) Application of fuzzy logic with genetic algorithms to FMEA method. ZESZYTY NAUKOWE POLITECHNIKI POZNAŃSKIEJ, Organizacja i Zarządzanie, Nr 62:5–20

3. Černý V (1985) Thermodynamical approach to the traveling salesman problem: an efficient simulation algorithm. J Optim Theory Appl 45(1):41–51

4. Chin K-S, Wang Y-M, Poon GKK, Yang J-B (2009) Failure mode and effects analysis by data envelopment analysis. Decis Support Syst 48(1):246–256

5. Dyer MK, Little DG, Hoard EG, Taylor EG, Campbell R (1972) Applicability of NASA contract quality management and failure mode effect analysis procedures to the USGS Outer Continental Shelf oil and gas lease management program

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