Research Article
Deterioration of Thermal Barrier Coated Turbine Blades by Erosion
Table 1
NASA-designed automotive turbine (TMX-71717) blade geometry.
| Blade row | Stator | Rotor |
| Pitch (cm) | 2.096 | 0.5621 | Mean chord (cm) | 2.311 | 1.043 | Height (cm) | 1.118 | 1.105 | L.E. radius (cm) | 0.0635 | 0.0331 | T.E. radius (cm) | 0.0191 | 0.0191 | Number of blades | 15 | 56 |
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