Snapshots of relative total pressure and deviation angle at rotor exit for two axial gaps Schematic of the vortex-vortex interaction Current turbomachinery architectures result in reduced stator-rotor axial gaps, amplifying the unsteady coupling between the stationary and rotating components. In this context, a number of research programs were carried out and are currently ongoing at … Leggi tutto Unsteady effects in Axial Turbine