Some early experimental results from a combined experimental and analytical study being conducted at NASA-Langley of the transonic flutter characterisitics of a generic arrow wing configuration are presented. The planned study includes the parametric variation of a variety of structural and geometric characteristics. Presented here are flutter results of the basic arrow wing, for the basic wing with the addition of two simulated lower-surface-mounted engine nacelles, and for the basic wing with the addition of both the fin and the engine nacelles.


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    Titel :

    Parametric Flutter Studies of an Arrow-Wing Configuration: Some Early Results


    Beteiligte:
    M. H. Durham (Autor:in) / S. R. Cole (Autor:in) / F. W. Cazier (Autor:in) / D. F. Keller (Autor:in) / E. C. Parker (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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