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A quasi-three-dimensional method for calculating blade surface velocities for an axial flow turbine bladeQuasi-three-dimensional compressible flow analysis for calculating blade surface velocities for axial flow turbine blade
Document ID
19660027753
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dellner, L. T. (NASA Lewis Research Center Cleveland, OH, United States)
Katsanis, T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-52234
Report Number: NASA-TM-X-52234
Accession Number
66N37043
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VELOCITY DISTRIBUTION
AXIAL FLOW
TURBINE BLADE

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