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Design and performance of controlled-diffusion stator compared with original double-circular-arc statorThe capabilities of two stators, one with controlled-diffusion (CD) blade sections and one with double-circular-arc (DCA) blade sections, were compared. A CD stator was designed and tested that had the same chord length but half the blades of the DCA stator. The same fan rotor (tip speed, 429 m/sec; pressure ratio, 1.65) was used with each stator row. The design and analysis system is briefly described. The overall stage and rotor performances with each stator are compared, as are selected blade element data. The minimum overall efficiency decrement across the stator was approximately 1 percentage point greater with the CD balde sections than with the DCA blade sections.
Document ID
19870017477
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gelder, Thomas F.
(NASA Lewis Research Center Cleveland, OH, United States)
Schmidt, James F.
(NASA Lewis Research Center Cleveland, OH, United States)
Suder, Kenneth L.
(NASA Lewis Research Center Cleveland, OH, United States)
Hathaway, Michael D.
(Army Aviation Systems Command Cleveland, Ohio., United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AVSCOM-TR-87-C-25
E-3694
NAS 1.15:100141
NASA-TM-100141
Report Number: AVSCOM-TR-87-C-25
Report Number: E-3694
Report Number: NAS 1.15:100141
Report Number: NASA-TM-100141
Accession Number
87N26910
Funding Number(s)
PROJECT: RTOP 535-05-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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