Fibre composite repair of cracked metallic aircraft components — practical and basic aspects
- 30 September 1987
- journal article
- Published by Elsevier in Composites
- Vol. 18 (4) , 293-308
- https://doi.org/10.1016/0010-4361(87)90293-x
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- 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
- A cracked plate repaired by bonded reinforcementsInternational Journal of Fracture, 1982
- An application of the inclusion analogy for bonded reinforcementsInternational Journal of Solids and Structures, 1981
- Thermal Considerations in the Patching of Metal Sheets with Composite OverlaysJournal of Structural Mechanics, 1980
- Finite Element Analysis of Patched CracksJournal of Structural Mechanics, 1979