NASA NTRS · 19680000097
Computer program calculates velocities and streamlines in turbomachines
Abstract
Computer program calculates the velocity distribution and streamlines over widely separated blades of turbomachines. It gives the solutions of a two dimensional, subsonic, compressible nonviscous flow problem for a rotating or stationary circular cascade of blades on a blade-to-blade surface of revolution.
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Katsanis, T.. 1968-05-01. Computer program calculates velocities and streamlines in turbomachines. https://ntrs.nasa.gov/citations/19680000097
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