Delamination in cross-ply laminated composite subjected to low-velocity impact
- 1 August 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (8) , 1498-1502
- https://doi.org/10.2514/3.11800
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A finite element calculation of stress intensity factors by a modified crack closure integralPublished by Elsevier ,2003
- A New Approach toward Understanding Damage Mechanisms and Mechanics of Laminated Composites Due to Low-Velocity Impact: Part I—ExperimentsJournal of Composite Materials, 1991
- Modelling of impact damage in composite laminatesComposites, 1989
- Initiation and extent of impact damage in graphite/epoxy and graphite/PEEK compositesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988