Research Article

Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio

Table 2

Variable range for 2D profile optimizations.

Suction surfacePressure surface
PositionRangePositionRange

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]