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    Titel :

    High Fidelity Flowpath Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets



    Kongress:

    47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL



    Erscheinungsdatum :

    2009-01-01


    Format / Umfang :

    13 pages


    Anmerkungen:

    Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    High Fidelity Flowpath Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets

    Malo-Molina, Faure / Gaitonde, Datta / Ebrahimi, Houshang et al. | AIAA | 2009


    Three-Dimensional Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets

    Malo-Molina, Faure J. / Gaitonde, Datta V. / Ebrahimi, Houshang B. et al. | AIAA | 2010




    Flowfield Structure in Generic Inward-Turning-Based Propulsion Flowpath Components

    Gaitonde, Datta / Malo-Molina, Faure / Croker, Barry et al. | AIAA | 2007