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

Figure 6

Computational and experimental spanwise distributions of total pressure ratio, total temperature ratio, adiabatic efficiency, and absolute flow angle at near-peak efficiency 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