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Computer program for calculating velocities and streamlines on a blade-to-blade stream surface of a turbomachineFORTRAN computer program for calculating two dimensional subsonic inviscid flow for rotating or stationary circular cascade of blades on blade to blade stream surface of turbomachine
Document ID
19680011905
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Katsanis, T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4525
Report Number: NASA-TN-D-4525
Accession Number
68N21374
Funding Number(s)
CONTRACT_GRANT: 720-03-01-35-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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