The effect of ply-drop configuration on the delamination strength oftapered composite structures
- 13 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Delamination of tapered composite structuresEngineering Fracture Mechanics, 1989
- Effect of dropped plies on the strength of graphite-epoxy laminatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Response and failure analysis of a graphite-epoxy laminate containing terminating internal pliesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985