The present, novel treatment of missile airframe-exhaust plume interactions emphasizes their simulation via a formal solution of the Reynolds-averaged Navier-Stokes (RNS) equation and is accordingly able to address the simulation requirements of novel missiles with nonconventional/integrated propulsion systems. The method is made possible by implicit RNS codes with improved artificial dissipation models, generalized geometric capabilities, and improved two-equation turbulence models, as well as by such codes' recent incorporation of plume thermochemistry and multiphase flow effects.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Exhaust plumes and their interaction with missile airframes - A new viewpoint


    Beteiligte:
    Dash, S. M. (Autor:in) / Sinha, N. (Autor:in)

    Erscheinungsdatum :

    01.01.1992


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch