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Analysis of fan-turbine efficiency characteristics in terms of size and stage numberRelationship between fan drive turbine geometry and output efficiency of turbofan engine
Document ID
19680013256
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Glassman, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Stewart, W. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1581
Report Number: NASA-TM-X-1581
Accession Number
68N22725
Funding Number(s)
CONTRACT_GRANT: 126-15-02-17-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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