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Radial inflow turbine performance with an exit diffuser designed for linear static pressure variationRadial inflow turbine performance with exit diffuser designed for linear static pressure variation
Document ID
19700032591
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)
Rohlik, H. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52890
Report Number: NASA-TM-X-52890
Accession Number
70N41907
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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