A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitudinal lateral stability characteristics of a general research model with the wing in a high position and a low position on the fuselage. The model had a wing with a quarter chord sweep of 42 deg, an aspect ratio of 6.78, a supercritical airfoil, and a high lift system which consisted of a leading edge slat and a double slotted flap. Various slat and flap deflections represented clean, take off, and landing configurations. A 45 deg swept horizontal tail located slightly below the fuselage center line was investigated with both the low and high wing configurations.


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    Titel :

    Effects of Wing Height on Low-Speed Aerodynamic Characteristics of a Model Having a 42 Deg Swept Wing, a Supercritical Airfoil, Double-Slotted Flaps, and a Low Tail


    Beteiligte:
    P. G. Fournier (Autor:in) / W. C. Sleeman (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    75 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch