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Computer program calculates velocities and streamlines in turbomachinesComputer program calculates the velocity distribution and streamlines over widely separated blades of turbomachines. It gives the solutions of a two dimensional, subsonic, compressible nonviscous flow problem for a rotating or stationary circular cascade of blades on a blade-to-blade surface of revolution.
Document ID
19680000097
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Katsanis, T.
Date Acquired
August 4, 2013
Publication Date
May 1, 1968
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-10252
Report Number: LEW-10252
Accession Number
68B10097
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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