A need to pump a mixture of two-phase fluid appears naturally in many situations. One example of this situation is aircraft fuel systems, where the pump inlet may have two-phase mixture due to the desorption of the dissolved gases at low pressures at higher altitudes. A simple procedure of selecting proper design conditions for the inlet inducer and a method of sizing the inducer, impeller and volute to meet all the design requirements has been described. This procedure has also been applied to a typical fighter plane boost pump design.


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    Titel :

    Sizing of an aircraft fuel pump


    Weitere Titelangaben:

    Auslegung einer Kraftstoffpumpe für Flugzeuge


    Beteiligte:
    Rohatgi, U.S. (Autor:in)


    Erscheinungsdatum :

    1995


    Format / Umfang :

    5 Seiten, 3 Bilder, 4 Tabellen, 14 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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