1. A direct linear-elastic analysis of double-symmetric bonded joints and reinforcements;Albat;Composites Science and Technology,1999
2. ANSYS Release 9.0., 2004. ANSYS Inc. Canonsburg, Pennsylvania, USA.
3. Arendt, C., Sun, C.T., 1994. Bending effects of asymmetric adhesively bonded composite repairs on cracked aluminum panels. In: Proceedings of the FAA/NASA International Symposium on Advanced Structural integrity for Airframe Durability and Damage Tolerance, NASA conference publication 3274, Part1, pp. 33–48.
4. Repair efficiency in fatigue-cracked aluminum components reinforced with boron/epoxy patches;Baker;Fatigue and Fracture of Engineering Materials and Structures,1993
5. Fatigue damage prediction for bonded composite repairs applied to metallic aircraft structures;Clark;SAE Journal of Aerospace,2001