Tests were conducted in the Langley 12-foot low-speed wind-tunnel to determine the longitudinal and lateral-directional aerodynamic effects of plain and tabbed vortex flaps on a flat-plate, highly swept arrow-wing model. Flow-visualization studies were made using a helium-bubble technique. Static forces and moments were measured over an angle-of-attack range from 0 deg to 50deg for sideslip angles of 0 deg and + or - 4 deg.


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    Title :

    Effects of vortex flaps on the low-speed aerodynamic characteristics of an arrow wing


    Contributors:
    Yip, L. P. (author) / Murri, D. G. (author)

    Publication date :

    1981-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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