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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Launch Environment Water Flow Simulations Using Smoothed Particle Hydrodynamics


    Beteiligte:
    B. T. Vu (Autor:in) / J. J. Berg (Autor:in) / M. F. Harris (Autor:in) / A. C. Crespo (Autor:in)

    Erscheinungsdatum :

    2015


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Launch Environment Water Flow Simulations Using Smoothed Particle Hydrodynamics

    Vu, Bruce T. / Berg, Jared J. / Harris, Michael F. et al. | NTRS | 2015


    Launch Environment Water Flow Simulation Using Smoothed Particle Hydrodynamics

    Vu, Bruce T. / Berg, Jared J. / Harris, Michael F. et al. | AIAA | 2015


    Launch Environment Water Flow Simulation Using Smoothed Particle Hydrodynamics (AIAA 2015-0049)

    Vu, Bruce T. / Berg, Jared J. / Harris, Michael F. et al. | British Library Conference Proceedings | 2015


    3D Wave Resistance Simulations Using Smoothed Particle Hydrodynamics

    Oger, G. / Doring, M. / Alessandrini, B. et al. | British Library Conference Proceedings | 2007


    Smoothed Particle Hydrodynamics for Water Waves

    Dalrymple, R.A. / Gomez-Gesteira, M. / Rogers, B.D. et al. | British Library Online Contents | 2010