Studies were conducted in research rocket motor burning premixed gases as propellants and effects of combustion chamber length, propellant equivalence ratio, mean chamber pressure and shape of nozzle upon longitudinal-mode pressure oscillations were examined; three modes of longitudinal pressure oscillations, namely, fundamental-, second harmonic- and third harmonic-mode oscillations were observed in combustion chamber and measured periods of each mode oscillation were found to satisfy relation of acousticmode oscillations; other findings.


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    Titel :

    Studies of high frequency combustion oscillations in gaseous propellant rocket motor


    Weitere Titelangaben:

    Tokyo Univ -- Aeronautical Research Inst -- Report


    Beteiligte:
    Tsuji, H. (Autor:in) / Takeno, T. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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