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Modeling Improvements and Users Manual for Axial-flow Turbine Off-design Computer Code AXODAn axial-flow turbine off-design performance computer code used for preliminary studies of gas turbine systems was modified and calibrated based on the experimental performance of large aircraft-type turbines. The flow- and loss-model modifications and calibrations are presented in this report. Comparisons are made between computed performances and experimental data for seven turbines over wide ranges of speed and pressure ratio. This report also serves as the users manual for the revised code, which is named AXOD.
Document ID
19950004441
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
August 1, 1994
Subject Category
Aerodynamics
Report/Patent Number
E-9052
NASA-CR-195370
NAS 1.26:195370
Report Number: E-9052
Report Number: NASA-CR-195370
Report Number: NAS 1.26:195370
Accession Number
95N10853
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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