Crack Deflection in Tungsten Carbide Based Laminates
Abstract
Laminate materials were manufactured by alternating WC-6%Co layers with equal thickness layers of one of the following compositions: WC-16%Co, WC-16%Ni, Co, a W-Ni-Fe alloy, and Ni. One composition used WC-6%Ni in place of WC-6%Co, layered with the W-Ni-Fe alloy. Flexure specimens, consisting of nine alternating layers, were fabricated with either WC-6%Co or WC-6%Ni on the tensile surface of the specimen. The ability of these composites to deflect or arrest cracks was investigated in four point bending. Two of the compositions, WC-6%Co/W-Ni-Fe and WC-6%Co/Ni, exhibited the ability to fail non-catastrophically, showing inelastic work of fracture as high as 34,400 J/m2.
Recommended Citation
J. L. Watts and G. Hilmas, "Crack Deflection in Tungsten Carbide Based Laminates," International Journal of Refractory Metals and Hard Materials, Elsevier Inc., Jan 2006.
The definitive version is available at https://doi.org/10.1016/j.ijrmhm.2005.04.005
Department(s)
Materials Science and Engineering
Keywords and Phrases
Crack Deflection; Fibrous Monolith; Laminate; Tungsten Carbide; Flexure
International Standard Serial Number (ISSN)
0263-4368
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2006 Elsevier Inc., All rights reserved.
Publication Date
01 Jan 2006