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    Titel :

    Numerical and Experimental Investigation of a Two-Staged Supersonic Combustion Chamber


    Beteiligte:

    Kongress:

    16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    01.01.2009




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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