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Calculating Flows In Multiple-Blade-Element CascadesComputer code written to analyze flows on blade-to-blade surfaces of turbomachinery. Analyzes rows containing blades of several different shapes and/or spacings. Capability makes code useful for calculating flows in centrifugal machinery with splitter blades or in mistuned blade rows, where blade spacing varies. Written primarily in FORTRAN IV.
Document ID
19880000044
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcfarland, Eric F. (NASA Lewis Research Center, Cleveland, Ohio.)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 1
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14359
Report Number: LEW-14359
ISSN: 0145-319X
Accession Number
88B10044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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