A delamination mechanism for thermal barrier coatings subject to calcium-magnesium-alumino-silicate (CMAS) infiltration

By C. Mercer, S. Faulhaber, A. G. Evans, R. Darolia. 2005

430 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Ceramics and Composites, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/1a615ce0d1e3c9144fa41dc258acc067ee708b7d

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. C. G. Levi
2. David R. Clarke
3. A. G. Evans
4. S. Krämer
5. C. Mercer
6. James Yang
7. J.R Williams
8. N. Padture

In Ceramics and Composites

1. C. G. Levi
2. David R. Clarke
3. A. G. Evans
4. R. Darolia

In Mechanical Engineering

1. C. G. Levi
2. David R. Clarke
3. A. G. Evans
4. C. Mercer
5. H. Wadley
6. V. Deshpande
7. J. W. Hutchinson
8. Norman A. Fleck

Citations in the corpus

• Infiltration‐Inhibiting Reaction of Gadolinium Zirconate Thermal Barrier Coatings with CMAS Melts (2008, background): “loss of insulation efficiency and accelerated degradation of the metallic layers underneath [ 14 ].”
• On a ferroelastic mechanism governing the toughness of metastable tetragonal-prime (t′) yttria-stabilized zirconia (2007, background): “The focus of this investigation is on the mode I toughness, directly pertinent to failure by erosion, FOD and CMAS degradation (Chen et al. 2003; Mercer et al. 2005).”
• CMAS degradation of environmental barrier coatings (2007, background): “exfoliation of the coating upon thermal cycling [6, 10 ].”