Aerodynamic characteristics obtained in a rotational flow environment utilizing a rotary balance located in a spin tunnel are presented in plotted form for a 1/6.5 scale, single engine, high wing, general aviation airplane model. The configurations tested included the basic airplane, various wing leading-edge devices, tail designs, and rudder control settings as well as airplane components. Data are presented without analysis for an angle of attack range of 8 deg to 90 deg and clockwise and counter-clockwise rotations covering an omega b/2V range from 0 to 0.85.


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    Titel :

    Rotary Balance Data for a Typical Single-Engine General Aviation Design for an Angle-of-Attack Range of 8 Deg to 90 Deg. 1: High-Wing Model B


    Beteiligte:
    W. Bihrle (Autor:in) / R. S. Hultberg (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    497 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch