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Computer program performs flow analysis through turbinesComputer program based on an equation for the velocity gradient along an arbitrary quasi- orthogonal analyzes flow through a turbomachine. The program obtains meridional solutions for a hub-to-shroud analysis and blade-to-blade analysis at the hub, mean, and shroud surfaces in a single computer run.
Document ID
19660000494
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Katsanis, T.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Electronic Components And Circuits
Report/Patent Number
LEW-236
Report Number: LEW-236
Accession Number
66B10496
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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