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    Titel :

    Subsonic wind tunnel tests on a crescent winged aircraft, including tests of leading edge droop designs and several tailplane heights


    Weitere Titelangaben:

    wind-tunnel crescent-winged leading-edge




    Erscheinungsdatum :

    1961


    Format / Umfang :

    61 S.


    Medientyp :

    Sonstige


    Format :

    Print


    Sprache :

    Englisch


    Klassifikation :

    RVK:    ZO 7000




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