The tests reported herein were made for the purpose of determining the high-speed load distribution on the wing of a 3/16 scale model of a scout-bomber airplane. Comparisons are made between the root bending-moment and section torsional-moment coefficients as obtained experimentally and derived analytically. The results show good correlation for the bending-moment coefficients but considerable disagreement for the torsional-moment coefficients.


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    Titel :

    High-Speed Load Distribution of the Wing of a 3/16 Scale Model of a Scout-Bomber Airplane with Flaps Deflected


    Beteiligte:
    R. H. Barnes (Autor:in)

    Erscheinungsdatum :

    1947


    Format / Umfang :

    89 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch