This paper describes the use of Smoothed Particle Hydrodynamics (SPH) to simulate the water flow from the rainbird nozzle system used in the sound suppression system during pad abort and nominal launch. The simulations help determine if water from rainbird nozzles will impinge on the rocket nozzles and other sensitive ground support elements.


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    Title :

    Launch Environment Water Flow Simulations Using Smoothed Particle Hydrodynamics


    Contributors:
    B. T. Vu (author) / J. J. Berg (author) / M. F. Harris (author) / A. C. Crespo (author)

    Publication date :

    2015


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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