Wind-tunnel tests to measure unsteady aerodynamic data in the transonic region have been completed on an aspect ratio 2.0 rectangular wing with a supercritical airfoil. The geometric and structural properties of the wing are presented. (Other references contain the measured aerodynamic data.) Both measured and design airfoil coordinates are presented and compared. In addition, measured wing bending and torsional stiffness distributions and some trailing-edge flexibility influence coefficients are presented.


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    Titel :

    Geometric and structural properties of a rectangular supercritical wing oscillated in pitch for measurement of unsteady transonic pressure distributions


    Beteiligte:
    Ricketts, R. H. (Autor:in) / Watson, J. J. (Autor:in) / Sandford, M. C. (Autor:in) / Seidel, D. A. (Autor:in)

    Erscheinungsdatum :

    1983-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Transonic pressure distributions on a rectangular supercritical wing oscillating in pitch

    Ricketts, R. H. / Sandford, M. C. / Seidel, D. A. et al. | NTRS | 1984


    Transonic pressure distributions on a rectangular supercritical wingoscillating in pitch

    RICKETTS, R. / SANDFORD, M. / SEIDEL, D. et al. | AIAA | 1983


    Transonic pressure distributions on a rectangular supercritical wingoscillating in pitch

    RICKETTS, R. H. / SANDFORD, M. C. / SEIDEL, D. A. et al. | AIAA | 1984


    Steady and unsteady transonic airloads on a supercritical wing

    RUO, S. Y. / MALONE, J. B. / HORSTEN, J. J. et al. | AIAA | 1985