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Radial in-flow turbine performance with exit diffusers designed for linear static pressure variationRadial-inflow turbine performance with exit diffusers designed for linear static-pressure variation
Document ID
19710022990
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kofskey, M. G. (NASA Lewis Research Center Cleveland, OH, United States)
Nusbaum, W. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
E-6276
NASA-TM-X-2357
Report Number: E-6276
Report Number: NASA-TM-X-2357
Accession Number
71N32466
Funding Number(s)
CONTRACT_GRANT: 120-27
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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