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Design and performance of a 427-meter-per-second-tip-speed two-stage fan having a 2.40 pressure ratioThe aerodynamic design and the overall and blade-element performances are presented of a 427-meter-per-second-tip-speed two-stage fan designed with axially spaced blade rows to reduce noise transmitted upstream of the fan. At design speed the highest recorded adiabatic efficiency was 0.796 at a pressure of 2.30. Peak efficiency was not established at design speed because of a damper failure which terminated testing prematurely. The overall efficiencies, at 60 and 80 percent of design speed, peaked at approximately 0.83.
Document ID
19780025166
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Cunnan, W. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Stevans, W.
(NASA Lewis Research Center Cleveland, OH, United States)
Urasek, D. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-9005
NASA-TP-1314
Report Number: E-9005
Report Number: NASA-TP-1314
Accession Number
78N33109
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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