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Flow Through a Rotating Turbomachinery Blade RowComputer program, QSONIC, developed for calculating full potential transonic quasi-three dimensional flow through rotating turbomachinery blade row. QSONIC written in FORTRAN IV.
Document ID
19830000102
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Farrell, C. A., Jr.
Date Acquired
August 11, 2013
Publication Date
August 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-13832
ISSN: 0145-319X
Report Number: LEW-13832
Accession Number
83B10102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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