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    Title :

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


    Conference:

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



    Publication date :

    2012-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    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