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    Titel :

    Helicopter Noise Measurements at High Advancing Blade Mach Number - A Novel Approach to Full Scale Flight Testing



    Kongress:

    International specialists' conference; 2nd, Aeromechanics ; 1995 ; Bridgeport; CT


    Erschienen in:

    Aeromechanics ; 5-84-5-94


    Erscheinungsdatum :

    1995-01-01


    Format / Umfang :

    80 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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