System consists of movable auxiliary aerodynamic sensors mounted on fuselage and connected to trailing-edge flaps by rigid mechanical linkages. System achieves alleviation by reducing lift-curve slope of airplane to such a small value that gust-induced angles of attack will result in small changes in lift.


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    Titel :

    Gust alleviation system to improve ride comfort of light airplanes


    Beteiligte:
    Stewart, E. C. (Autor:in) / Phillips, W. H. (Autor:in) / Hewes, D. E. (Autor:in)

    Erscheinungsdatum :

    1975-10-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Analysis of gust-alleviation system for transport airplanes

    Nakagawa, K. | Engineering Index Backfile | 1964


    Gust alleviation

    Phillips, W. H. | NTRS | 1971


    Gust Loads on Airplanes

    Rhode, Richard V. | SAE Technical Papers | 1937