Connection between oscillatory propellant flow and HF combustion instability in rocket motors and theoretical treatment for describing flow in fuel pipe lines under transient or oscillatory conditions; method of characteristics is developed in way similar to that employed in 1-dimensional gas dynamic studies; diagrams constructed are position and state diagram; methods used for calculations.


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    Titel :

    Method of calculating liquid flow fluctuations in rocket motor supply pipes


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Woods, W.A. (Autor:in)

    Erschienen in:

    ARS Journal ; 31 , n 11


    Erscheinungsdatum :

    1961


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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