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    Titel :

    NUMERICAL DESIGN STUDY OF SCRAMJET ISOLATOR CROSS-SECTIONAL SHAPE TRANSITION WITH VARIED DIVERGENCE ANGLE



    Kongress:

    16th, International symposium on air breathing engines ; 2003 ; Cleveland, Ohio



    Erscheinungsdatum :

    01.01.2003


    Format / Umfang :

    1252 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






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