The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating characteristics of bi-phase propellant rocket combustors operating at sub-critical conditions. Both analytical and experimental work were performed in order to study the aforementioned problems. (Author)


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    Title :

    Parametric Study of Rocket Instability


    Contributors:
    J. R. Osborn (author) / D. W. Netzer (author)

    Publication date :

    1968


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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