Experiments made at Purdue Univ Jet Propulsion Center to determine factors which contribute to occurrence of transverse modes of combustion pressure oscillation in rocket motors; results indicated that changes in aspect ratio and volume of rocket motor combustion chamber had profound effect on incidence and amplitude of transverse modes determined to be "spinning" and radial modes.


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    Title :

    Importance of combustion chamber geometry in high frequency oscillations in rocket motors


    Additional title:

    ARS J


    Contributors:

    Published in:

    ARS Journal ; 31 , n 4


    Publication date :

    1961


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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