A one-dimensional analysis of pressure and velocity-coupled driving of a standing wave is presented. In the model it is assumed that each incremental propellant surface area is a possible source of combustion driven wavelets. The wavelets are separated into components in phase or 90 degrees out-of-phase with the standing wave and the driving obtained by summing up the in-phase response over the complete burning surface.


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    Titel :

    Axial Mode, Intermediate Frequency Combustion Instability in Solid Propellant Rockets


    Beteiligte:
    G. L. Dehority (Autor:in) / E. W. Price (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    81 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch