An experimental investigation was conducted to determine the drag coefficient of particles in flow regimes encountered in a rocket nozzle. The acquisition of these data leads to more reliable predictions of nozzle performance inefficiencies owing to gas-particle flow. The Mach number-Reynolds number regime traversed by a particle in a rocket nozzle is described. (Author)


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    Title :

    Measurement of Particle Drag Coefficients in Flow Regimes Encountered by Particles in a Rocket Nozzle


    Contributors:

    Publication date :

    1968


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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