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NASA NTRS · 20000021273

Durability of Ceramic Matrix Composites in Combustion Environments

Abstract

SiO2 scale volatility and the resulting recession of SiC has been previously identified for CVD, as well as sintered, SiC and Si3N4 materials. Linear weight loss and surface recession of SiC was observed as a result of SiO2 volatility for both fuel-lean and fuel-rich gas mixtures. A strong Arrhenius temperature dependence exist and parametric studies using multiple linear regression were used to develop recession relationships as a function of e(sup -Q/RT) central dot P(sup X)V(sup y) for both lean and rich combustion conditions. Recession of 0.2 - 2.0 micron/hr is predicted for typical combustion conditions at 1200 - 1400 C, with a somewhat higher absolute recession rate and activation energy for rich combustion versus lean.

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BibTeXRIS

Robinson, Raymond C., Smialek, James L.. 1999-01-01. Durability of Ceramic Matrix Composites in Combustion Environments. https://ntrs.nasa.gov/citations/20000021273

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