Research Article
Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio
Table 2
Variable range for 2D profile optimizations.
| | Suction surface | Pressure surface | | Position | Range | Position | Range |
| | 0 | [-0.5,0.5] | 0 | [-0.5,0.5] | | 0.15 | [-0.5,0.5] | 0.15 | [-0.5,0.5] | | 0.30 | [-0.5,0.5] | 0.30 | [-0.5,0.5] | | 0.50 | [-0.5,0.5] | 0.50 | [-0.5,0.5] | | 0.70 | [-0.5,0.5] | 0.70 | [-0.5,0.5] | | 0.85 | [-0.5,0.5] | 0.85 | [-0.5,0.5] | | 1.00 | [-0.5,0.5] | 1.00 | [-0.5,0.5] |
|
|