Damage Tolerance of Aircraft Panels Taking into Account Residual Stress

Author:

Richter-Trummer V.,Moreira P. M. G. P.,de Castro P. M. S. T.

Publisher

Springer Berlin Heidelberg

Reference61 articles.

1. Wanhill, R.J.H.: Milestone case histories in aircraft structural integrity. In: Milne, I., Ritchie, R.O., Karihaloo, B. (eds.) Comprehensive Structural Integrity, vol. 1, pp. 61–72. Elsevier. ISBN:0-08-044157-2

2. Schijve, J.: Fatigue damage in aircraft structures, not wanted, but tolerated? Int. J. Fatigue 31, 998–1011 (2009)

3. Brot, A., Peleg-Wolfin, Y.: The damage-tolerance behavior of intregrally stiffened metallic structures. In: 48th Israel Annual Conference on Aerospace Sciences IACAS Conference (2008)

4. National Transportation Safety Board – NTSB. Aircraft Accident Report, Aloha Airlines, Flight 243, Boeing 737-200, N73711, Near Maui, Hawaii, April 28, 1988. National Transport Safety Board, Washington, DC (1989)

5. Boller, C., Buderath, M.: Fatigue in aerostructures—where structural health monitoring can contribute to a complex subject. Philos. Trans. R. Soc. A 365, 561–587 (2007)

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