Crack growth and repair of multi-site damage of fuselage lap joints
- 31 March 1993
- journal article
- Published by Elsevier in Engineering Fracture Mechanics
- Vol. 44 (4) , 627-637
- https://doi.org/10.1016/0013-7944(93)90103-y
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspectsComposite Structures, 1989
- Increasing the fatigue life of cracked fastener holes using bonded repairsTheoretical and Applied Fracture Mechanics, 1989
- Repair of mirage III aircraft using the BFRP crack-patching techniqueTheoretical and Applied Fracture Mechanics, 1984