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    Titel :

    Numerical analysis of rocket turbopump inducer at cryogenic homogeneous two-phase flow conditions


    Beteiligte:
    Akmandor, I. (Autor:in) / Nagashima, Toshio (Autor:in)

    Kongress:

    37th Aerospace Sciences Meeting and Exhibit ; 1999 ; Reno , NV , U.S.A.



    Erscheinungsdatum :

    01.01.1999



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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