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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    Titel :

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


    Beteiligte:
    C. T. Crowe (Autor:in) / W. R. Babcock (Autor:in) / P. G. Willoughby (Autor:in) / R. L. Carlson (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    60 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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