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Enhanced capabilities and updated users manual for axial-flow turbine preliminary sizing code TURBANSeveral modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbine cooling has been added to the analysis. New alternative input options allow direct specification of stage reaction, stage work factor, and stage work split. The Reynolds number loss dependency was modified and an internal calculation of air viscosity was added. A complete description of input and output along with sample cases are included.
Document ID
19950009497
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glassman, Arthur J.
(Toledo Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:195405
E-9252
NASA-CR-195405
Report Number: NAS 1.26:195405
Report Number: E-9252
Report Number: NASA-CR-195405
Accession Number
95N15912
Funding Number(s)
PROJECT: RTOP 505-69-50
CONTRACT_GRANT: NAG3-1165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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