Fatigue crack growth predictions in Aramid reinforced aluminum laminates (ARALL)
- 1 February 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (2), 135-140
- https://doi.org/10.2514/3.45553
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Flight simulation behaviour of aramid reinforced aluminium laminates (ARALL)Engineering Fracture Mechanics, 1984
- A cracked plate repaired by bonded reinforcementsInternational Journal of Fracture, 1982