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Project TitleRTOD Radial Turbine Off-Design Performance Code
Track CodeLEW-14060
DescriptionCode RTOD predicts the performance of a single-stage radial-inflow turbine (with either radial or swept rotor blades) as a function of pressure ratio, speed, and stator setting. The program models the flow with stator viscous and trailing-edge losses, a vaneless-space loss, and rotor incidence, viscous, training-edge, clearance, and disk friction losses. The stator-inlet and exit and rotor-inlet flows, each of which are at constant radius, are modeled by a meanline analysis, but sector analysis is used at the rotor exit. For a pivoting stator, the leakage flow through the clearance gap is accounted for.
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RTOD - Contains Execute, Samples Request Key

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