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    Titel :

    AIAA-2005-1267 SURGE MARGIN IMPROVEMENT OF MULTISTAGE TRANSONIC COMPRESSOR USING CFD



    Kongress:

    17th, International symposium on air breathing engines ; 2005 ; Munich, Germany



    Erscheinungsdatum :

    01.01.2005


    Format / Umfang :

    225 pages


    Anmerkungen:

    Includes bibliographical references and index; Papers on CD-ROM



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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