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Estimation of Requirements of Inspection Intervals for Panels Susceptible to Multiple Site Damage

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Structural Integrity of Aging Airplanes

Part of the book series: Springer Series in Computational Mechanics ((SSCMECH))

Summary

The objectives of the work reported in this paper were to assess the probability of detection of Multi-Site Damage (MSD) in fuselage lap-splices in aging airplanes. The results indicate that a reduction in the mandated period between inspections should be considered. Perforce, the model had to rely on NDI inspection reliability measured on samples devoid of MSD. A recommendation is made for a program to acquire such data for MSD.

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References

  1. D. Broek, “The feasibility of proof testing”, FractuREsearch Inc., Report to the Transportation Systems Center (1989).

    Google Scholar 

  2. W.H. Lewis et al, “Reliability of non-destructive inspection”, San Antonio Air Logistics Center, Report SA-ALC/MME 76-6-38-1 (1978).

    Google Scholar 

  3. S. Patil, Finite element analysis of lap joint. Foster-Miller Inc. (1990).

    Google Scholar 

  4. A. Hartman, “Fatigue tests on 3-row lap-joints in clad 2024-T3 manufactured by riveting and adhesive bonding”, Nat. Aerospace Lab., NLR, Amsterdam, Report TN M-2170 (1967).

    Google Scholar 

  5. J. Schijve, “The endurance under program fatigue testing”, in Full-Scale Fatigue Testing of Aircraft Structures, pp 41-59, Pergamon (1961).

    Google Scholar 

  6. L. Jarfall “Review of some Swedish work on fatigue of aircraft structures during 1975–1977”, Institute for Aviation Research, FFA, Stockholm, Report TN HE-1918.

    Google Scholar 

  7. T. Haas, “Spectrum fatigue tests on typical wing joints”, Material Pruefung 2 (1960), 1, pp 117.

    Google Scholar 

  8. D. Broek, The Practical Use of Fracture Mechanics, Kluwer Ac. Publ., (1988).

    Google Scholar 

  9. D.P. Rooke and D.J. Cartwright, Compendium of Stress Intensity Factors, HM Stationery Office, London (1976).

    Google Scholar 

  10. D. Broek, Elementary Engineering Fracture Mechanics, Kluwer Ac. Publ. 4th edition (1986).

    Google Scholar 

  11. D. Broek, “Fracture control by periodic inspection with fixed cumulative probability of crack detection, in Structural Failure, Product Liability and Technical Insurance”, Rossmanith Ed. pp 238-258, Interscience Ent. (1987).

    Google Scholar 

  12. D. Broek, USAF ASIP Conference, Dayton (1986).

    Google Scholar 

  13. E. Knor, “Reliability of the detection of flaws and of the determination of flaw size”, AGARDograph 176, pp 396–412 (1974).

    Google Scholar 

  14. Anon, Software for damage tolerance analysis, FractuREsearch Inc. (1989).

    Google Scholar 

  15. U. Gorenson, Paper presented at ICAF meeting Toulouse (1983).

    Google Scholar 

  16. R. Mayville, “A Laboratory Study of Fracture in the Presence of Lap-Splice Multiple Site Damage”, Presented at the International Symposium on Stuctural Integrity of Aging Airplanes, Atlanta, Georgia (1990).

    Google Scholar 

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© 1991 Springer-Verlag Berlin, Heidelberg

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Sampath, S., Broek, D. (1991). Estimation of Requirements of Inspection Intervals for Panels Susceptible to Multiple Site Damage. In: Atluri, S.N., Sampath, S.G., Tong, P. (eds) Structural Integrity of Aging Airplanes. Springer Series in Computational Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-84364-8_23

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  • DOI: https://doi.org/10.1007/978-3-642-84364-8_23

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-84366-2

  • Online ISBN: 978-3-642-84364-8

  • eBook Packages: Springer Book Archive

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