Effect of ply-drop configuration on delamination strength of tapered composite structures
- 1 August 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 34 (8) , 1650-1656
- https://doi.org/10.2514/3.13285
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- The Effect of Film Adhesive on the Delamination Strength of Tapered CompositesJournal of Composite Materials, 1992
- Tailoring concepts for improved structural performance of rotorcraft flexbeamsComposites Engineering, 1992
- Structural Tailoring Techniques to Prevent Delamination in Composite LaminatesJournal of the American Helicopter Society, 1990
- Delamination of tapered composite structuresEngineering Fracture Mechanics, 1989
- Delamination Control of Composite Rotor HubsJournal of the American Helicopter Society, 1986
- Response and failure analysis of a graphite-epoxy laminate containing terminating internal pliesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Experimental and Analytical Studies On the Onset of Delamination in Laminated CompositesJournal of Composite Materials, 1984
- Stress Fracture Criteria for Laminated Composites Containing Stress ConcentrationsJournal of Composite Materials, 1974