New mathematical model for leakage flow around shrouded turbopump inducers yields more realistic analyses from which designers determine best geometry for leakage-flow-reinjection ports. Also, designers use calculated velocity profile at inducer leading edge to determine blade-angle distribution of inducer leading edge.
Calculating Leakage Around Turbopump Inducer Shrouds
NASA Tech Briefs ; 11 , 4
1987-04-01
Sonstige
Keine Angabe
Englisch
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