Engineering methods to calculate unsteady airloads on wings in transonic flow were applied in flutter calculations for a semispan flutter model of a supercritical wing. A verification was performed by comparing flutter characteristics, and the prediction of transonic dips in the flutter boundaries. When applied complementary, the methods produce useful results.


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    Titel :

    Verification of Calculation Methods for Unsteady Airloads in the Precipitation of Transonic Flutter


    Beteiligte:
    R. J. Zwaan (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch