Biaxial and Triaxial Failure Strengths of 6061-T6 Aluminum and AS4/3501-6 Carbon/Epoxy Laminates Obtained by Testing Thickness-Tapered Cruciform Specimens
Authors:
- Ea ArmaniosEAEa Armanios
- Rb BucinellRBRb Bucinell
- Dw WilsonDWDw Wilson
- Js WelshJWJs Welsh
- Df AdamsDADf Adams
- 1 January 2001
- journal article
- Published by ASTM International in Journal of Composites Technology and Research
- Vol. 23 (2) , 111
Abstract
No abstract availableKeywords
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- Response of Quasi-Isotropic Carbon/Epoxy Laminates to Biaxial StressJournal of Composite Materials, 1986