Probabilistic Model of Multiple-Site Fatigue Damage of Riveting in Airframes

Author:

Ignatovich S. R.

Publisher

Springer Science and Business Media LLC

Subject

Mechanics of Materials

Reference21 articles.

1. J. Schijve, “Multiple-site damage in aircraft fuselage structures,” Fatigue Fract. Eng. Mater. Struct., 18, No. 3, 329–344 (1995).

2. W. R. Hendricks, “The Aloha airlines accident – a new era for aging aircraft,” in: S. N. Atluri, S. G. Sampath, and P. Tong (Eds.), Structural Integrity of Aging Airplanes, Springer-Verlag, Berlin–Heidelberg (1991), pp. 153–166.

3. Method of Determining the Consistency with AP 25.571. Provision of Safety of the Construction as Regards the Strength during Long-Term Operation [in Russian], Mintrans, Moscow (1996).

4. Recommendations for Regulatory Action to Prevent Widespread Fatigue Damage in the Commercial Airplane Fleet: a Report of the AAWG (Final Report), Airworthiness Assurance Working Group (1999).

5. C. Boller, “Structural health management of ageing aircraft and other infrastructure,” in: Structural Health Monitoring, Institute of Smart Structures and Systems (ISSS), Bangalore, India (2002), pp. 1–59.

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