Yaw control and overall efficiency increased at hover and low speeds. Wind-tunnel investigation showed strake located on left side of tail boom has potential to reduce high adverse side loads on tail boom in hover and in sideward flight. Test demonstrated addition of single long strake to left side of tail boom most effective configuration for reducing left pedal requirements in right sideward flight.


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    Titel :

    Helicopter Tail-Boom Strakes


    Beteiligte:
    Kelley, H. L. (Autor:in) / Phelps, A. E., III (Autor:in) / Wilson, J. C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1986-06-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Further Research On Helicopter Tail-Boom Strakes

    Kelley, Henry L. / Crowell, Cynthia A. / Yenni, Kenneth R. et al. | NTRS | 1994



    Flight investigation of the effect of tail boom strakes on helicopter directional control

    Kelley, Henry L. / Crowell, Cynthia A. / Yenni, Kenneth R. et al. | NTRS | 1990


    Flight Investigation of the Effect of Tail Boom Strakes on Helicopter Directional Control

    H. L. Kelly / C. A. Crowell / K. R. Yenni et al. | NTIS | 1993