1. Fracture analysis of adhesively bonded cracked panels;Swift;J Eng Mater Technol Trans ASME,1978
2. Vlieger H. Residual strength of bonded stiffened panels: prediction and experimental verification. Nationaal Lucht-en Ruimtevaartlaboratorium, Verslagen en Verhandeling. Report TR 83066U, 1983.
3. Poe Jr. CC. Tensile strength of composite sheets with unidirectional stringers and crack-like damage. ACEE Composite Structures Technology - Review of Selected NASA Research on Composite Materials and Structures, NASA CP-2321, 1984, p. 97–111.
4. Important considerations in commercial aircraft damage tolerance;Swift;Int J Vehic Des,1986
5. Rans CD, Alderliesten RC. Damage tolerance philosophy for bonded aircraft structures. In: Bos MJ, editor. Bridging the Gap between Theory and Operational Practice. Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Springer-Verlag, 2009, p. 73–90.