Abstract
Thermal cycling of a platinum modified, nickel aluminide (Ni,Pt)Al coated single crystal superalloy, between 1000 and 1150 °C with 10 min holds at each temperature, and subject to a compressive uniaxial stress is reported. There are two major effects of the superimposed compressive stress not observed in the absence of the stress. One is that the rumpling pattern exhibits an asymmetry with an increase of the bond coat surface roughness perpendicular to the applied loading axis. The other is the formation of cracks in the thermally grown oxide aligned parallel to the stress axis.
| Original language | English |
|---|---|
| Pages (from-to) | 2321-2327 |
| Number of pages | 7 |
| Journal | Acta Materialia |
| Volume | 57 |
| Issue number | 7 |
| DOIs | |
| State | Published - Apr 2009 |
| Externally published | Yes |
Funding
This work was supported by the Office of Naval Research under Contract A00014-04-1-0053. The authors are grateful to Dr. Ken Murphy, Howmet Research Corporation for supplying the materials studied in this work.
Keywords
- Coating
- Cyclic oxidation testing
- Grain structure
- Profilometry
- Rumpling