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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Dill, D.G. (Autor:in) / Lamoree, M.D. (Autor:in) / Melching, F.W. (Autor:in) / Stringham, R.H. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1954 Flutter



    Erscheinungsdatum :

    1954


    Format / Umfang :

    24 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :