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.
Stalled-Flow and Head-Loss Model for Diffuser Pumps
NASA Tech Briefs ; 8 , 2
1984-11-01
Sonstige
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Englisch
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