An Experimental Evaluation of Static Strength and Fatigue Life on Composite Patch Repaired AA2024-T4 Plate
Author:
Affiliation:
1. Rajaas Engineering College
2. University College of Engineering
3. St. Xavier's Catholic College of Engineering
Abstract
Publisher
Trans Tech Publications, Ltd.
Subject
General Engineering
Link
https://www.scientific.net/AMR.984-985.233.pdf
Reference15 articles.
1. A.A. Baker, Bonded Composite Repair of Metallic Aircraft Components-Overview of Australian Activities, AGARD – Compos Repair of Military Aircraft Struct (1995) (1) 1-14.
2. T. E. Tay, F. S. Chau, C. J. Er., Bonded boron-epoxy composite repair and reinforcement of cracked aluminium structures. Compos Struct 34 (1996) 339-347.
3. Alan Baker, Bonded composite repair of fatigue-cracked primary aircraft structure, Compos Struct 47 (1999) 431-443.
4. Ki-Hyun Chung, Won-Ho Yang, A study on the fatigue crack growth behavior of thick aluminum panels repaired with a composite patch, Compos Struct 60 (2003) 1–7.
5. Jones R, Chiu WK, Sawyer JPG, Composite repairs to cracks in thick metallic components. Compos Struct (1999) 44(1): 17–29.
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