The report shows that the yaw-rate effect of the gust produces considerable low-frequency attenuation of the airframe side-gust response which would be neglected by considering the sideslip effect alone.


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    Titel :

    Airplane Yaw Perturbations due to Vertical and Side Gusts


    Beteiligte:
    R. R. Rankine (Autor:in) / C. T. Leondes (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    3 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airplane Yaw Perturbations due to Vertical and Side Gusts

    ROBERT R. RANKINE AND CORNELIUS T. LEONDES | AIAA | 1972


    Airplane design for gusts

    Houbolt, J. C. | NTRS | 1977



    Theory of an airplane encountering gusts II

    Wilson, Edwin Bidwell | NTRS | 1918


    Theory of an Airplane Encountering Gusts III

    Wilson, Edwin Bidwell | NTRS | 1918