NASA NTRS · 19830000196
Axial Compressor Design and Analysis
Abstract
Program 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.
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William, J. G., Hearsay, R. M.. 1983-10-01. Axial Compressor Design and Analysis. https://ntrs.nasa.gov/citations/19830000196
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