RTD Radial-Inflow Turbine Conceptual Design Code(LEW-17453-1)

system testing
RTD Radial-Inflow Turbine Conceptual Design Code
(LEW-17453-1)
Overview
The RTD code executes a conceptual design for a single-stage radial-inflow turbine. A mean-line analysis is performed for the locations having constant radius over the blade span. Constant span-fraction sectors are used at the rotor exit. The analysis can account for stator end-wall clearance flow and swept rotor blades. The loss model includes stator and rotor passage losses, trailing-edge losses, vaneless space loss, disk-friction loss, and rotor-exit clearance loss.
Software Details

Category
System Testing
Reference Number
LEW-17453-1
Release Type
U.S. Release Only
Operating System
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