Problem of determining stability is treated as perturbation of classical acoustics problem; analysis is developed for stability of stationary pressure waves in chambers using either liquid or gaseous propellants; formulation is for 3-dimensional case; computations are carried out for cylindrical chamber in which mean flow velocity is parallel to axis and varies only with axial position.


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    Title :

    Stability of high-frequency pressure oscillations in rocket combustion chambers


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 1 , n 5


    Publication date :

    1963


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :