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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    Title :

    Axial Mode, Intermediate Frequency Combustion Instability in Solid Propellant Rockets


    Contributors:

    Publication date :

    1974


    Size :

    81 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English