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Analytical determination of radial inflow turbine design geometry for maximum efficiencyOptimum design geometry for high radial inflow turbine performance efficiency
Document ID
19680006474
Document Type
Other - NASA Technical Note (TN)
Authors
Rohlik, H. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1968
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-4384
Accession Number
68N15943
Funding Number(s)
CONTRACT_GRANT: 120-27-03-13-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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