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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    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    45 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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