Fracture analysis of multi-site cracking in fuselage lap joints
- 1 September 1994
- journal article
- Published by Springer Nature in Computational Mechanics
- Vol. 13 (5) , 315-331
- https://doi.org/10.1007/bf00512586
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- A hybrid finite element method for damage tolerance analysisComputers & Structures, 1984
- Stress intensity factors for some through-cracked fastener holesInternational Journal of Fracture, 1975
- Strain energy release rate for radial cracks emanating from a pin loaded holeInternational Journal of Fracture, 1972