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Axial Compressor Design and AnalysisProgram yields blade configurations and aerodynamic flow fields. Program consists of three sections -- two blade design sections and aerodynamic section Program structured that one section used alone, or aerodynamic section used in conjunction with either or both of blading sections. Program written in FORTRAN IV.
Document ID
19830000196
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
William, J. G. (University of Dayton)
Hearsay, R. M.
Date Acquired
August 11, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13488
Accession Number
83B10196
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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