| Article ID | Journal | Published Year | Pages | File Type | 
|---|---|---|---|---|
| 7896513 | Corrosion Science | 2013 | 11 Pages | 
Abstract
												The performances of a ZrB2-SiC-LaB6 ultra-high temperature ceramic (UHTC) was investigated in high enthalpy supersonic air flow. The UHTC material reached and maintained steady-state radiative surface temperature of 1973 K (monitored by pyrometer) for 5 min, and survived the arc-jet plasma exposure without any optical evidence of mechanical damage. The oxide scale covering externally the sample evolved into different textures. Transient thermal analysis processed via CFD provided a good agreement between the numerical steady-state temperature and the temperature distribution obtained experimentally. The contemporary addition of LaB6 and SiC to ZrB2 had a detrimental effect on the overall oxidation resistance.
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											Authors
												Frédéric Monteverde, Davide Alfano, Raffaele Savino, 
											