Refractory diborides of zirconium and hafnium
Journal of the American Ceramic Society, ISSN: 0002-7820, Vol: 90, Issue: 5, Page: 1347-1364
2007
- 1,879Citations
- 84Usage
- 649Captures
- 2Mentions
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
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Metrics Details
- Citations1,879
- Citation Indexes1,879
- 1,879
- CrossRef1,613
- Usage84
- Abstract Views84
- Captures649
- Readers649
- 649
- Mentions2
- References2
- 2
Article Description
This paper reviews the crystal chemistry, synthesis, densification, microstructure, mechanical properties, and oxidation behavior of zirconium diboride (ZrB2) and hafnium diboride (HfB2) ceramics. The refractory diborides exhibit partial or complete solid solution with other transition metal diborides, which allows compositional tailoring of properties such as thermal expansion coefficient and hardness. Carbothermal reduction is the typical synthesis route, but reactive processes, solution methods, and pre-ceramic polymers can also be used. Typically, diborides are densified by hot pressing, but recently solid state and liquid phase sintering routes have been developed. Fine-grained ZrB2 and HfB2 have strengths of a few hundred MPa, which can increase to over 1 GPa with the addition of SiC. Pure diborides exhibit parabolic oxidation kinetics at temperatures below 1100°C, but B2O3 volatility leads to rapid, linear oxidation kinetics above that temperature. The addition of silica scale formers such as SiC or MoSi2 improves the oxidation behavior above 1100°C. Based on their unique combination of properties, ZrB2 and HfB2 ceramics are candidates for use in the extreme environments associated with hypersonic flight, atmospheric re-entry, and rocket propulsion. © 2007 The American Ceramic Society.
Bibliographic Details
http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=34248350351&origin=inward; http://dx.doi.org/10.1111/j.1551-2916.2007.01583.x; https://ceramics.onlinelibrary.wiley.com/doi/10.1111/j.1551-2916.2007.01583.x; https://scholarsmine.mst.edu/matsci_eng_facwork/480; https://scholarsmine.mst.edu/cgi/viewcontent.cgi?article=1479&context=matsci_eng_facwork; http://doi.wiley.com/10.1111/j.1551-2916.2007.01583.x; https://onlinelibrary.wiley.com/doi/abs/10.1111/j.1551-2916.2007.01583.x
Wiley
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