Mechanical properties and interlaminar toughness of cross-plied laminates containing adhesive strips
- 1 February 1991
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (2), 247-252
- https://doi.org/10.2514/3.10571
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Effect of Adhesive Layers on Impact Damage in Composite LaminatesPublished by ASTM International ,1988
- Optimal Use of Adhesive Layers in Reducing Impact Damage in Composite LaminatesPublished by Springer Nature ,1987
- Characterization of Mode I and Mixed-Mode Failure of Adhesive Bonds Between Composite AdherendsPublished by ASTM International ,1986
- Improvement of Edge Delamination Strength of Composite Laminates Using Adhesive LayersPublished by ASTM International ,1986
- Delamination Resistant Composite ConceptsPublished by ASTM International ,1986
- Impact Induced Fracture in a Laminated CompositeJournal of Composite Materials, 1985
- Determination of GIC in Angle Ply Composites Using a Cantilever Beam Test MethodJournal of Reinforced Plastics and Composites, 1983
- Microscopic Observations of Cross Sections of Impacted Composite LaminatesJournal of Composites Technology and Research, 1982