Mechanical behavior and failure mechanisms of boron carbide based three-layered laminates with weak interfaces
Abbreviated Journal Title
Ceram. Int.
Keywords
Laminate; Ceramics; Fracture toughness; Residual stress; STRESS INTENSITY FACTOR; FRACTURE-TOUGHNESS; CERAMIC COMPOSITES; RESISTANCE; DESIGN; Materials Science, Ceramics
Abstract
The effect of weak interfaces on failure mechanisms of a three-layered composite was studied. Three-layered B(4)C/B(4)C-C(nanofibers) laminates have been produced using a hot pressing technique. The laminates were designed with thick (similar to 2.6 mm) outer layers of B(4)C and a thin (similar to 90 mu m) center layer of B(4)C-70 wt.% C(nanofibers). Based on the difference in coefficients of thermal expansion and Young's moduli of the pure B(4)C and B(4)C-70 wt.% C(nanofibers) layers, it was estimated that low tensile thermal residual stress with a magnitude of 11.3 +/- 2.5 MPa was developed in the thick B(4)C outer layers, and compressive residual stress with a magnitude of 455.7 +/- 5 MPa was developed in the thin central B(4)C-70 wt.% C(nanofibers) layer. The apparent fracture toughness of laminates was measured and based on the estimated fracture toughness values, a threshold stress was calculated. (C) 2011 Elsevier Ltd and Techna Group S.r.l. All rights reserved.
Journal Title
Ceramics International
Volume
37
Issue/Number
7
Publication Date
1-1-2011
Document Type
Article
Language
English
First Page
2255
Last Page
2261
WOS Identifier
ISSN
0272-8842
Recommended Citation
"Mechanical behavior and failure mechanisms of boron carbide based three-layered laminates with weak interfaces" (2011). Faculty Bibliography 2010s. 1597.
https://stars.library.ucf.edu/facultybib2010/1597
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