An experimental investigation was conducted to determine the effect of the mixing of gaseous propellants on high-frequency combustion pressure oscillations in a rocket motor. The results indicate the influence of the type of injector, some mixing parameters (injection velocity and momentum flux ratio), the combustion pressure, and the propellant combination. (Author)


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    Title :

    Combustion Pressure Oscillations in an Unmixed Gas Rocket Motor


    Contributors:

    Publication date :

    1966


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English