1976, Zeszyt 70-72
Abstract
To characterize the supersonic flow at the outlet of transsonic cascades blade turbines were tested for gas flow in the nozzle inclined delimited by straight lines. It was assumed that the floating fluid is non-viscous, allowing the existence of waves uderzeniolvych causing an increase in entropy.
In addition, it is assumed that the flow at the inlet nozzle is uniform.
Keywords:
supersonic flow, floating fluid, entropy