Airplane under consideration is high aspect ratio, transonic bomber from which turbojet engines are suspended in nacelles below wings; chief difficulties were in accurately predicting wing torsional frequencies and in adequately representing nacelle pylon characteristics; adequate analysis is possible when these are properly taken into account.


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    Title :

    Comparison of experimental and analytical flutter characteristics for swept wing jet bomber


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1954 Flutter



    Publication date :

    1954


    Size :

    24 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :