1. Bonded repair of aircraft structures;Baker,1988
2. Repair efficiency in fatigue cracked aluminum components reinforced with boron/epoxy patches;Baker;Fatigue Fract. Engng. Mater. Struct.,1993
3. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch;Denney;Engng. Fract. Mech.,1997
4. Fredell RS. Damage tolerant repair techniques for pressurized aircraft fuselages. Ph.D. Dissertation, Faculty of Aerospace Engineering, Delft University of Technology, Delft, The Netherlands, 1994
5. Kan HP, Ratwani MM. Composite patch repair of thick aluminum structures-final report. Airtask no.WF41-400, PE 62241. Report no. NADC-82139-60. United States Navy-Naval Air Development Center, Warminster, PA 18974, 1983