Unsteady aerodynamic loads in the transonic domain were obtained with time-linearized methods in which a so-called field panel method which accounts for a proper radiation of signals towards infinity is embedded. The methods are used to predict the unsteady loads and first harmonic pressure distributions on an airfoil and a transport type wing. Results are correlated with data of unsteady experiments and of other calculation methods. Transonic flutter applications to a fighter-type configuration are described.


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    Titel :

    Application of Time-Linearized Methods of Oscillating Wings in Transonic Flow and Flutter


    Beteiligte:
    M. H. L. Hounjet (Autor:in) / J. J. Meijer (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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