Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Performance of Choked Unsteady Ejector-Nozzles for use in Pressure Gain Combustors



    Kongress:

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



    Erscheinungsdatum :

    01.01.2009


    Format / Umfang :

    9 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






    Ejector Enhanced Pulsejet Based Pressure Gain Combustors: An Old Idea with a New Twist

    Paxson, D. E. / Dougherty, K. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2005


    Cryogenic homogeneous two-phase flows in choked Laval nozzles

    Akmandor, I. / Nagashima, Toshio | AIAA | 1998


    Cryogenic Homogeneous Two-Phase Flows in Choked Laval Nozzles

    Akmandor, I. S. / Nagashima, T. / AIAA | British Library Conference Proceedings | 1998