Biaxial and Triaxial Failure Strengths of 6061-T6 Aluminum and AS4/3501-6 Carbon/Epoxy Laminates Obtained by Testing Thickness-Tapered Cruciform Specimens
- 1 January 2001
- journal article
- Published by ASTM International in Journal of Composites Technology and Research
- Vol. 23 (2), 111
- https://doi.org/10.1520/ctr10919j
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Failure envelopes for notched CSM laminates under biaxial loadingComposites, 1995
- Optimal design of biaxial tensile cruciform specimensJournal of the Mechanics and Physics of Solids, 1993
- Response of Quasi-Isotropic Carbon/Epoxy Laminates to Biaxial StressJournal of Composite Materials, 1986