Mathematical analysis developed which couples mass transport in rocket chamber with energy transport in solid propellant; one-dimensional model proposed considers sinusoidal perturbations, allowing for exponential growth of disturbance; analysis uses energy balance for burning solid propellant that accounts for energy accumulation in solid and mass balance on rocket chamber that considers mass accumulation in gas chamber; resultant equations are subjected to perturbation analysis with final form reducing to expression relating frequency of nonacoustic oscillations to characteristic length of chamber; data were obtained with AP-PBAA propellant containing 5% aluminum.


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    Titel :

    Nonacoustic instability of composite propellant combustion


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Beckstead, M.W. (Autor:in) / Ryan, N.W. (Autor:in) / Baer, A.D. (Autor:in)

    Erschienen in:

    AIAA Journal ; 4 , n 9


    Erscheinungsdatum :

    1966


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :