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Quasi-three-dimensional calculation of velocities in turbomachine blade rowsA practical way of obtaining an approximation to a three dimensional flow is to combine several two-dimensional solutions (quasi-three-dimensional solution). Three basic types are discussed of two-dimensional solutions (meridional, blade-to-blade, and channel) and several ways of combining them. A centrifugal impeller is analyzed as an example. All recommended methods are based on available NASA general purpose computer programs.
Document ID
19720025109
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Katsanis, T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
E-6666
NASA-TM-X-67959
Report Number: E-6666
Report Number: NASA-TM-X-67959
Meeting Information
Meeting: Winter Ann. Meeting of the ASME
Location: New York
Start Date: November 12, 1972
End Date: November 16, 1972
Accession Number
72N32759
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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