Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Computation of Transverse Injection into Supersonic Crossflow with Various Injector Orifice Geometries


    Contributors:

    Conference:

    42nd AIAA Aerospace Sciences Meeting and Exhibit



    Publication date :

    2004-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Computation of Transverse Injection into Supersonic Crossflow with Various Injector Orifice Geometries

    Foster, L. E. / Engblom, W. A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004


    TRANSVERSE INJECTION INTO SUBSONIC CROSSFLOW WITH VARIOUS INJECTOR ORIFICE GEOMETRIES

    Foster, L. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010



    Computational Investigation of Fuel Injection with Various Injector Geometries and Mixing into Hypersonic Crossflow in Scramjet Engines

    Ogawa, H. / Boyce, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013