1. Bonded repair of aircraft structure,1988
2. Baker AA. Fatigue crack propagation studies on aluminium panels patched with boron/epoxy composite. In: Jones R, Miller NJ, editors. International conference on aircraft damage assessment and repair, Melborn, Australia, 1991, p. 209–15.
3. Analysis of cracked adhesively bonded laminated structures;Ratwani;AIAA J,1979
4. A cracked plate repaired by bonded reinforcements;Rose;Int J Fract,1982
5. An assessing method of fatigue life on central-through cracked plate with adhesive bounded reinforcement, fatigue, fracture, and risk;Lu;ASME,1991