Research Article
Deterioration of Thermal Barrier Coated Turbine Blades by Erosion
Table 2
Operating conditions for NASA-designed turbine.
| Parameters | NASA 1979 design automotive turbine TMX-71717 |
| Inlet total temperature | 1325 (K) | Inlet total pressure | 3.92 (atm) | Mass flow rate | 0.598 (kg/s) | Rotor speed | 6126.9 (rad/s) | Shaft power | 22.615 (kW) | Reaction | 0.8013 | Total-to-total polytrophic efficiency % | 78.5385 |
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