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Flow velocities and streamlinesComputer program calculates subsonic or transonic flow on hubshroud, midchannel, stream surface of single-blade row of turbomachine. Program uses finite-different and quasi-orthogonal (velocity-gradient) methods. Program is reported in two volumes: Part I is User's Manual, Part II is Programmer's Manual.
Document ID
19780000094
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Katsanis, T.
Mcnally, W. D.
Date Acquired
August 9, 2013
Publication Date
June 1, 1978
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-12966
Report Number: LEW-12966
ISSN: 0145-319X
Accession Number
78B10094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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