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Computer program calculates transonic velocities in turbomachinesComputer program, TSONIC, combines velocity gradient and finite difference methods to obtain numerical solution for ideal, transonic, compressible flow for axial, radial, or mixed flow cascade of turbomachinery blades.
Document ID
19710000399
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Katsanis, T.
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-10977
Report Number: LEW-10977
Accession Number
71B10402
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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