Multiple-Site Damage in Riveted Lap Joints – Experimental Observations

Author:

Skorupa Andrzej,Skorupa Małgorzata

Publisher

Springer Netherlands

Reference32 articles.

1. Ahmed, A., Bakuckas, J.G., Jr., Tan, P.W., Awerbuch, J., Lau, A.C., Tan, T.-M.: Growth of multiple-site damage (MSD) in an undamaged fuselage lap joint curved panel. In: Proceedings of 7th Joint FAA/DoD/NASA Conference on Aging Aircraft, New Orleans, LA, 8–11 Sept 2003 (2003)

2. Ahmed, A., Bakuckas, J.G., Jr., Averbuch, J., Lau, A.C., Tan, T.-M.: Evolution of multiple-site damage in the riveted lap joint of fuselage panel. In: Proceedings of 8th Joint NASA/FAA/DoD Conference on Aging Aircraft, Palm Springs, CA, Jan 31–Feb 3 2005 (2005)

3. Aircraft Accident Report, Aloha Airlines, Flight 243, Boeing 737–200, N73711, near Manui, Hawaii, April 28, 1988, Report No. NTSB/AAR-89/03. National Transportation Safety Board, Washington, D.C. (June 1989)

4. Bakuckas, J.G., Jr.: Full-scale testing and analysis of fuselage structures containing multiple cracks. Final Report, DOT/FAA/AR-01/46 (July 2002)

5. Bakuckas, J.G., Jr., Bigelow, C.A., Tan, P.W.: Characterization of fatigue behaviour of aircraft fuselage structures. In: Guillaume, M. (ed.) Proceedings of 22nd ICAF Symposium, Fatigue of Aeronautical Structures as an Engineering Challenge, Lucerne, Switzerland, 7–9 May 2003, pp. 341–360. EMAS, Warley (2003)

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