Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    STUDY OF DUAL-MODE FLOWFIELD IN SCRAMJET COMBUSTOR


    Beteiligte:

    Kongress:

    39th, Aerospace sciences meeting ; 2001 ; Reno, NV



    Erscheinungsdatum :

    2001-01-01


    Format / Umfang :

    ALL


    Anmerkungen:

    Paper nos AIAA-2001-0003 to AIAA-2001-0660 with gaps


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Dual-mode flowfield in scramjet combustor

    Abdel-Salam, T. / Tiwari, S. / Mohieldin, T. | AIAA | 2001


    Study of dual-mode flowfield in scramjet combustor

    Tiwari, S. / Abdel-Salam, T. / Chaturvedi, S. et al. | AIAA | 2001


    Numerical Study of a Dual-Mode Combustor Flowfield

    Abdel-Salam, Tarek / Tiwari, S / Mohieldin, T. | AIAA | 2002


    Influence of Turbulence Modelling on Combustor Flowfield in Scramjet Mode of RBCC Engine

    Salloum, Joseph / Candon, Michael / Ogawa, Hideaki et al. | AIAA | 2020


    INFLUENCE OF TURBULENCE MODELLING ON COMBUSTOR FLOWFIELD IN SCRAMJET MODE OF RBCC ENGINE

    Salloum, Joseph / Candon, Michael / Ogawa, Hideaki et al. | TIBKAT | 2020