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INVESTIGATION OF A 0.6 HUB-TIP RADIUS-RATIO TRANSONIC TURBINE DESIGNED FOR SECONDARY-FLOW STUDY. III - EXPERIMENTAL PERFORMANCE WITH TWO STATOR CONFIGURATIONS DESIGNED TO ELIMINATE BLADE WAKES AND SECONDARY-FLOW EFFECTS AND CONCLUSIONS FROM ENTIRE STATOR INVESTIGATIONHub-tip radius ratio transonic turbine for secondary flow - stator configurations designed to eliminate blade wakes and secondary-flow effects
Document ID
19630002670
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Moffitt, T. P. (NASA Lewis Research Center Cleveland, OH, United States)
Rohlik, H. E. (NASA Lewis Research Center Cleveland, OH, United States)
Wintucky, W. T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
September 17, 1957
Subject Category
Aircraft
Report/Patent Number
NACA-RM-E57G08
Report Number: NACA-RM-E57G08
Accession Number
63N12546
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER
TURBINE
STATOR
WAKE
HUB-TIP RATIO
AIRFLOW
TRANSONIC FLOW

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