Engineering Application of an Identification Method to Shock-Induced Vortex Stability in the Transonic Axial Fan Rotor

Figure 7

Computational and experimental spanwise distributions of total pressure ratio, total temperature ratio, adiabatic efficiency, and absolute flow angle at near stall condition.

(a) Spanwise distribution of total pressure ratio

(b) Spanwise distribution of total temperature ratio

(c) Spanwise distribution of adiabatic efficiency

(d) Spanwise distribution of absolute flow angle