Small perturbation analysis on stability of conservation of mass in solid-propellant combustor is made for LF regime; to avoid unwieldy model, dynamics of concentrated combustion zone are represented parametrically in terms of magnitude and phase of combustion oscillations relative to pressure oscillations; resulting model is susceptible to easy interpretation in terms of trends among oscillation variables, combustor variables, and propellant combustion characteristics; experimental data obtained are presented.


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    Titel :

    Nonacoustic combustor instability


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Beckstead, M.W. (Autor:in) / Price, E.W. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 11


    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Nonacoustic combustor instability.

    Beckstead, M. W. / Price, E. W. | NTRS | 1967


    Nonacoustic combustor instability.

    BECKSTEAD, M. W. / PRICE, E. W. | AIAA | 1967



    Nonacoustic instability of composite propellant combustion

    Beckstead, M.W. / Ryan, N.W. / Baer, A.D. | Engineering Index Backfile | 1966