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Project TitleTurban Turbomachine design code
Track CodeLEW-17454
DescriptionThe TURBAN analysis is performed at the arithmetic-mean diameter. The stage velocity diagrams are either all similar (thereby having the same work factor) or are determined from an input stage work split. All stages have the same stator exit angle. Stage by stage tailoring of the velocity diagrams is not allowed. Only inlet and exit diameters are input, and continuity is performed only at the first-stage exit and turbine exit. The loss model is a simple viscous type related to the velocity diagrams.
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Turban - Contains Execute, Samples Request Key

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