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

Figure 12

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

(a) Radial distribution of total pressure ratio

(b) Radial distribution of total temperature ratio

(c) Radial distribution of adiabatic efficiency