Effects of stacking sequence on microscopic fatigue damage development in quasi-isotropic CFRP laminates with interlaminar-toughened layers
- 23 June 1999
- journal article
- Published by Elsevier in Composites Science and Technology
- Vol. 59 (9) , 1387-1398
- https://doi.org/10.1016/s0266-3538(98)00180-8
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Microscopic fatigue failure process in interleaved and toughness-improved CFRP cross-ply laminatesAdvanced Composite Materials, 1997
- Experimental Characterization of Microscopic Damage Initiation and Growth in Quasi-Isotropic CFRP Laminates.TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series A, 1996
- Microscopic fatigue damage progress in CFRP cross-ply laminatesComposites, 1995
- An analytic model for thermoelastic properties of composite laminates containing transverse matrix cracksInternational Journal of Solids and Structures, 1993
- A Conceptual Framework for the Interpretation of Fatigue Damage Mechanisms in Composite MaterialsJournal of Composites Technology and Research, 1985
- Fatigue of composite materials: damage mechanisms and fatigue-life diagramsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1981