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FORTRAN program for predicting off-design performance of radial-inflow turbinesThe FORTRAN IV program uses a one-dimensional solution of flow conditions through the turbine along the mean streamline. The program inputs needed are the design-point requirements and turbine geometry. The output includes performance and velocity-diagram parameters over a range of speed and pressure ratio. Computed performance is compared with the experimental data from two radial-inflow turbines and with the performance calculated by a previous computer program. The flow equations, program listing, and input and output for a sample problem are given.
Document ID
19750024045
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Wasserbauer, C. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Glassman, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8368
NASA-TN-D-8063
Accession Number
75N32118
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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