NASA NTRS · 19830000673
Stalled-Flow and Head-Loss Model for Diffuser Pumps
Abstract
Modeling procedure approximates inlet transition zone (blade leading edge to blade throat) of diffuser pump as two-dimensional cascade, properties of which are well known. Model applied to stators as well as rotors. Procedure much faster than previous methods.
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Meng, S. Y.. 1984-11-01. Stalled-Flow and Head-Loss Model for Diffuser Pumps. https://ntrs.nasa.gov/citations/19830000673
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