The model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over an angle-of-attack range of -4 deg to 24 deg and over a sideslip range of plus or minus 8 deg at thrust coefficients of 0, 0.14, and 0.30. Control effectiveness and hinge moments were taken on the aileron, elevator, and rudder for a full range of deflections. Downwash measurements at the tail were obtained for the range of thrust coefficient and flap deflection. (Author)


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    Titel :

    Wind Tunnel Investigation of Static Longitudinal and Lateral Characteristics of a Full Scale Mockup of a Light Single Engine High Wing Airplane


    Beteiligte:
    H. D. Greer (Autor:in) / J. P. Shivers (Autor:in) / M. P. Fink (Autor:in) / C. R. Carter (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    158 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch