Structural Tailoring Techniques to Prevent Delamination in Composite Laminates
- 1 October 1990
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 35 (4) , 38-45
- https://doi.org/10.4050/jahs.35.38
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Quadratic Stress Criterion for Initiation of DelaminationJournal of Composite Materials, 1988
- Prevention of free-edge delamination via edge alterationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Suppression of edge delamination in composite laminates by terminating a critical ply near the edgesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Delamination Control of Composite Rotor HubsJournal of the American Helicopter Society, 1986
- Improvement of Edge Delamination Strength of Composite Laminates Using Adhesive LayersPublished by ASTM International ,1986
- The Use of Stitching to Suppress Delamination in Laminated CompositesPublished by ASTM International ,1985
- Hybrid Finite Element Analysis of Free Edge Effect in Symmetric Composite LaminatesPublished by Defense Technical Information Center (DTIC) ,1983
- Analysis of Free Edge Induced Failure of Composite LaminatesPublished by Springer Nature ,1979