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    Titel :

    The Gas Turbine Engine Conceptual Design Process - An Integrated Approach



    Kongress:

    Symposium, Design principles and methods for aircraft gas turbine engines ; 1998 ; Toulouse; France



    Erscheinungsdatum :

    01.01.1999


    Format / Umfang :

    1 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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