Computer code determines rotor exit flow from hub to tip. RTOD (Radial Turbine Off-Design), computes off-design performance of radial turbine by modeling flow with stator viscous and trailing-edge losses, and with vaneless space loss between stator and rotor, and with rotor incidence, viscous, clearance, trailing-edge, and disk friction losses.
Off-Design Performance of Radial-Inflow Turbines
NASA Tech Briefs ; 9 , 3
1986-01-01
Miscellaneous
No indication
English
Design analysis of radial-inflow turbines
NTRS | 1977
|Aerodynamic performance of radial inflow turbines ; 1
TIBKAT | 1964
Applications and Performance Levels of Radial Inflow Turbines
SAE Technical Papers | 1964
|