Research Article

Research on Aerodynamic Optimization Method of Multistage Axial Compressor under Multiple Working Conditions Based on Phased Parameterization Strategy

Table 1

Performance comparison at multiple conditions before and after optimization.

Working pointFlow rate (kg/s)Total pressure ratioAdiabatic efficiency (%)Surge margin (%)

Original (N = 1.0)112.13.5482.110.2
Optimized (N = 1.0)111.43.5482.415.9
Relative change−0.6%0.0%+0.3+5.7
Original (N = 0.8)86.452.4783.428.2
Optimized (N = 0.8)86.052.4784.826.7
Relative change−0.5%0.0%+1.4−1.5