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Channel Flow AnalysisThe design of a proper blade profile requires calculation of the blade row flow field in order to determine the velocities on the blade surfaces. An analysis theory is presented for several methods used for this calculation and associated computer programs that were developed are discussed.
Document ID
19740025365
Acquisition Source
Legacy CDMS
Document Type
Other - Technical Report
Authors
Theodore Katsanis (Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Turbine Design and Application: Volume 2
Publisher: National Aeronautics and Space Administration
Subject Category
Numerical Analysis
Accession Number
74N33478
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19740025363Collected WorksTurbine Design and Application: Volume 2
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