Flutter calculations were based on modified strip-analysis method of N ACA Research Memo L57L10 and covered Mach numbers from 0 to 1.75; flutter suppressor consists of small mass connected to wing by means of flexible sting; 3 suppressor masses were investigated but no attempt was made to make configuration optimum.


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    Titel :

    Theoretical investigation of subsonic and supersonic flutter characteristics of swept wing employing tuned sting-mass flutter suppressor


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1960


    Format / Umfang :

    45 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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