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Analytical and experimental investigation of stator endwall countouring in a small axial-flow turbineAn experimental and analytical investigation was conducted to determine the effect of stator endwall contouring on turbine stage performance. In this investigation three stator configurations were evaluated using a common rotor. The three stator configurations were a cylindrical endwall design and two contoured endwall designs, one having a S-shaped outer wall profile and the other having a conical-shaped outer wall profile. Experimental data were obtained over a range of equivalent speeds, total pressure ratios, and rotor tip clearances for each stator-rotor combination. Detailed analytical loss assessments were conducted to aid in the determination of the contouring effect on turbine performance.
Document ID
19840024318
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Haas, J. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Boyle, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-2050
NAS 1.60:2309
NASA-TP-2309
AVSCOM-TR-84-C-5
Report Number: E-2050
Report Number: NAS 1.60:2309
Report Number: NASA-TP-2309
Report Number: AVSCOM-TR-84-C-5
Accession Number
84N32388
Funding Number(s)
PROJECT: RTOP 535-05-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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