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Detailed flow measurements in casing boundary layer of 429-meter-per-second-tip-speed two-stage fanDetailed flow measurements between all blade rows were taken in the outer 30 percent of passage height of a two stage fan. Tabulations of the detailed flow measurements are included. Results of these measurements revealed the steep axial velocity profiles near the casing. The axial velocity profile near the casing at the rotor exists was much steeper than at the stator exits. The data also show overturning of the flow at the tip at the stator exits. The effect of mixing is shown by the redistribution of the first stage rotor exit total temperature profile as it passes through the following stator.
Document ID
19840020726
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Gorrell, W. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.60:2052
NASA-TP-2052
E-219
AVRADCOM-TR-81-C-28
Report Number: NAS 1.60:2052
Report Number: NASA-TP-2052
Report Number: E-219
Report Number: AVRADCOM-TR-81-C-28
Accession Number
84N28795
Funding Number(s)
PROJECT: RTOP 505-32-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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