Deterioration of Thermal Barrier Coated Turbine Blades by Erosion

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="601837.fig.0011a" src="https://static.hindawi.com/articles/ijrm/volume-2012/601837/figures/601837.fig.0011a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Commercial turbine   </td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="601837.fig.0011b" src="https://static.hindawi.com/articles/ijrm/volume-2012/601837/figures/601837.fig.0011b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>NASA-designed turbine </td></tr></table></td></tr></table>

<table>Mach number contours at the 50% blade span.</table>

International Journal of Rotating Machinery

fig11

Figure 11

Figure 11: Deterioration of Thermal Barrier Coated Turbine Blades by Erosion 