Numerical analysis of rocket turbopump inducer at cryogenic homogeneous two-phase flow conditions
37th Aerospace Sciences Meeting and Exhibit ; 1999 ; Reno , NV , U.S.A.
01.01.1999
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Analysis of Rocket Turbopump Inducer at Cryogenic Homogeneous Two-phase Flow Conditions
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