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Effects of four inlet and outlet tip-annulus-area blockage configurations on the performance of an axial-flow fan rotorAn axial-flow fan rotor was tested with four configurations of tip-annulus-area blockage to speeds as high as 0.8 of design speed. The rotor performance with the four blockage configurations is compared with the unblocked rotor performance and with blockage configurations previously investigated. The blockage configurations enable the rotor to operate in a stable condition, to much lower flows than the unblocked rotor, with no evidence of rotating stall. The blockage configurations were effective in reducing rotor torque and weight flow but were accompanied by reductions in pressure ratio and efficiency.
Document ID
19760008930
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Osborn, W. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Hager, R. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-8131
E-8466
Report Number: NASA-TN-D-8131
Report Number: E-8466
Accession Number
76N16018
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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