Numerical Simulation of Fatigue Crack Growth in A Pre-Cracked Thin Plate Repaired With A FRP Patch
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-15-4779-9_23
Reference24 articles.
1. Baker AA, Callinan RJ, Davis MJ, Jones R, Williams JG (1984) Repair of MIRAGE III Aircraft using the BFRP crack patching technique. Theor Appl Frac Mech 2:1–15
2. Baker AA (1987) Fibre composite repair of cracked metallic aircraft components-practical and basic aspects. Composites 18(4):293–308
3. Baker Alan (1999) Bonded composite repair of fatigue-cracked primary aircraft structure. Compos Struct 47:431–443
4. Domazet Z (1996) Comparison of fatigue crack retardation methods. Eng Fail Anal 3(2):137–147
5. Shinde PS, Kumar P, Singh KK, Tripathi VK, Sarkar PK (2015) Experimental Study of CFRP patches bonded on a cracked aluminum alloy panel. Compos Interfaces 22(4):233–248
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