Strength Predictions of Composite Laminates with Unloaded Fastener Holes
- 1 May 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (5) , 585-589
- https://doi.org/10.2514/3.50790
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Stress Fracture Criteria for Laminated Composites Containing Stress ConcentrationsJournal of Composite Materials, 1974