Abstract
A carbon fiber-reinforced silicon carbide matrix composite with pyrolytic carbon interface (Cf-PyC/SiC) and a protective coating was prepared by isothermal low pressure chemical vapor infiltration. Low-cycle fatigue behavior of this material system was investigated at high temperatures up to 1800°C in a combustion environment and at room temperature in air, respectively. The combustion environment includes thermal mechanical loading, high temperatures, and oxidizing atmosphere. Low-cycle fatigue tests were conducted at a maximum stress level of 180 MPa but at various temperatures and fatigue cycles. The residual strength variation of fatigue-survived samples was due to different damage mechanisms in different environments.
| Original language | English |
|---|---|
| Pages (from-to) | 491-499 |
| Number of pages | 9 |
| Journal | International Journal of Applied Ceramic Technology |
| Volume | 12 |
| Issue number | 3 |
| DOIs | |
| State | Published - 1 May 2015 |
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