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

Table 4

Variable position and range for 3D blade optimizations.

The central arc of the profile		Chord length		Profile installation angle
Relative chord position	Range/relative maximum thickness	Position/relative blade height	Range/relative chord length	Position/relative blade height	Range/degree
0	[-0.5,0.5]	0	[-0.1,0.1]	0	[-3.0,3.0]
0.25	[-0.5,0.5]	0.25	[-0.1,0.1]	0.25	[-2.5,2.5]
0.50	[-0.5,0.5]	0.50	[-0.1,0.1]	0.50	[-2.0,2.0]
0.75	[-0.5,0.5]	0.75	[-0.1,0.1]	0.75	[-1.5,1.5]
1.00	[-0.5,0.5]	1.00	[-0.1,0.1]	1.00	[-1.0,1.0]