NASA NTRS · 19710000399
Computer program calculates transonic velocities in turbomachines
Abstract
Computer program, TSONIC, combines velocity gradient and finite difference methods to obtain numerical solution for ideal, transonic, compressible flow for axial, radial, or mixed flow cascade of turbomachinery blades.
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Katsanis, T.. 1971-10-01. Computer program calculates transonic velocities in turbomachines. https://ntrs.nasa.gov/citations/19710000399
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