1. A review of some damage tolerance design approaches for aircraft structures;Toor;Eng. Fract. Mech.,1973
2. Fracture analysis of adhesively bonded cracked panels;Swift;J. Eng. Mater. Technol.,1978
3. Crack stoppers and arall laminates;Schijve;Eng. Fract. Mech.,1990
4. M. Heinimann, R. Bucci, M. Kulak, M. Garratt, Improving damage tolerance of aircraft structures through the use of selective reinforcement, in: Proceedings of the 23rd Symposium of International Committee on Aeronautical Fatigue, ICAF 2005, Hamburg, 2005, pp. 197–208.
5. Analytical prediction model for fatigue crack propagation and delamination growth in glare;Alderliesten;Int. J. Fatigue,2007