The reinforcing effect of composite patch repairs on metallic aircraft structures
- 31 January 1992
- journal article
- Published by Elsevier in International Journal of Adhesion and Adhesives
- Vol. 12 (1) , 19-26
- https://doi.org/10.1016/0143-7496(92)90004-f
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- The evaluation of non-tank surface treatments for aluminium bonding repairsInternational Journal of Adhesion and Adhesives, 1992
- Composite patch reinforcement of cracked aircraft upper longeron: analysis and specimen simulationTheoretical and Applied Fracture Mechanics, 1990
- Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspectsComposite Structures, 1989
- Isoparametric shear spring element applied to crack patching and instabilityTheoretical and Applied Fracture Mechanics, 1989
- Fibre composite repair of cracked metallic aircraft components — practical and basic aspectsComposites, 1987
- Repair of mirage III aircraft using the BFRP crack-patching techniqueTheoretical and Applied Fracture Mechanics, 1984
- Repair of cracked or defective metallic aircraft components with advanced fibre composites—an overview of Australian workComposite Structures, 1984
- Neutral axis offset effects due to crack patchingComposite Structures, 1983