The reinforcing effect of composite patch repairs on metallic aircraft structures
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Abstract
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Research context
OpenAlex topics: Fire effects on concrete materials · Fatigue and fracture mechanics · Mechanical Behavior of Composites
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References (22)
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1. Repair of cracked or defective metallic aircraft components with advanced fiber composites — an overview of Australian work10.1016/0263-8223(84)90025-4 ↗
2. Repair of Mirage III aircraft using the BFRP crack-patching technique10.1016/0167-8442(84)90035-1 ↗
3. Fibre composite repair of cracked metallic aircraft components — practical and basic aspects10.1016/0010-4361(87)90293-X ↗
4. Development of composite patches to repair complex cracked metallic structures
5. Composite repair of cracked aluminium alloy aircraft structure
6. Baker · 1988
7. Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting structural aspects10.1016/0263-8223(89)90030-5 ↗
8. Ong, C.L., Shu, W.Y. and Shen, S.B. ‘The evaluation of non-tank surface treatments for aluminium bonding repairs’ Int J Adhesion and Adhesives (submitted)10.1016/0143-7496(92)90027-S ↗
9. The development of adhesive bonding technology for aircraft structures (III)
10. The study on the advanced composite reinforcement to aircraft structures
11. Isoparametric shear spring element applied to crack patching and instability10.1016/0167-8442(89)90037-2 ↗
12. Adhesive-bonded composite-patching repair of cracked aircraft structure
13. Composite patch reinforcement of cracked aircraft upper longeron: analysis and specimen simulation10.1016/0167-8442(90)90040-7 ↗
14. Composite-patching repair of an aircraft nosedome
15. The composite-patching reinforcement of an aluminum casting missile structure
16. Neutral axis offset due to crack patching10.1016/0263-8223(83)90010-7 ↗
17. Chang · 1981 · Vol 1
18. Adhesive Bonding
19. Field-level repair materials and processes
20. Repair of Adhesive Bonded Aerospace Structures
21. F-5E/F.T.O., (Northrop, CA, USA, 1985) 1F-5E-3, 10–16, 10–19
22. F-104 T.O., (Lockheed, CA, USA, 1985) 1F104-3, 4-196C, 4-196D