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Comparison of Experimental and Analytical Performance for Contoured Endwall StatorsComparisons between predicted and experimental stator losses showed that the analysis was able to predict the change in stator loss when contoured endwalls with highly three dimensional passage geometry were used. The level of loss was predicted to within 75 percent of that measured. The predicted loss was due only to profile loss and boundary layer growth on the endwalls. The 25 percent difference was approximately 0.015 at design pressure ratio. The analysis was shown to predict the trend in stator flow angle, even for small stator geometries.
Document ID
19820018423
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boyle, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Haas, J. E.
(Army Aviation Research and Development Command Cleveland, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AVRADCOM-TR-82-C-12
NASA-TM-82877
NAS 1.15:82877
Report Number: AVRADCOM-TR-82-C-12
Report Number: NASA-TM-82877
Report Number: NAS 1.15:82877
Accession Number
82N26299
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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