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    Titel :

    Shock tunnel and numerical studies of a large inlet-fuelled inward turning axisymmetric scramjet


    Kongress:

    18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    01.01.2012




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    SHOCK TUNNEL AND NUMERICAL STUDIES OF A LARGE INLET-FUELLED INWARD TURNING AXISYMMETRIC SCRAMJET

    Boyce, R.R. / Schramm, J.M. / Oberg, D. et al. | British Library Conference Proceedings | 2012


    Scramjet Combustor Analysis Integrated to an Innovative Inward Turning Inlet

    Malo-Molina, Faure / Gaitonde, Datta / Ebrahimi, Houshang et al. | AIAA | 2008


    Investigation of the Effects of Lateral Cowl Length in an Inward Turning Scramjet Inlet

    Rolim, T. / Lu, F.K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013