Wing leading-edge deflection effects on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration were determined. Static force tests were conducted in a V/STOL tunnel at a Reynolds number of about 2.5 x 1 million for an angle-of-attack range from -10 deg to 17 deg and an angle-of-sideslip range from -5 deg to 5 deg. Limited flow visualization studies were also conducted in order to provide a qualitative assessment of leading-edge upwash characteristics.


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    Title :

    Effects of Wing Leading-Edge Deflection on the Low-Speed Aerodynamic Characteristics of a Low-Aspect-Ratio Highly Swept Arrow-Wing Configuration


    Contributors:
    P. L. Coe (author) / R. P. Weston (author)

    Publication date :

    1978


    Size :

    70 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English