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Off-Design Performance of Radial-Inflow TurbinesComputer 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.
Document ID
19850000402
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Meitner, P. L.
Glassman, A. J.
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14060
Accession Number
85B10402
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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