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Performance of two-stage fan with larger dampers on first-stage rotorThe performance of a two stage, high pressure-ratio fan, having large, part-span vibration dampers on the first stage rotor is presented and compared with an identical aerodynamically designed fan having smaller dampers. Comparisons of the data for the two damper configurations show that with increased damper size: (1) very high losses in the damper region reduced overall efficiency of first stage rotor by approximately 3 points, (2) the overall performance of each blade row, downstream of the damper was not significantly altered, although appreciable differences in the radial distributions of various performance parameters were noted, and (3) the lower performance of the first stage rotor decreased the overall fan efficiency more than 1 percentage point.
Document ID
19790015796
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Urasek, D. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Cunnan, W. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Stevans, W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8958
NASA-TP-1399
Report Number: E-8958
Report Number: NASA-TP-1399
Accession Number
79N23967
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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