Low speed wind tunnel data show that wings of aspect ratios 3 and 4 can produce maximum lift coefficients twice that of conventional double-slotted flap configurations by using powered high lift systems. These high lift systems, which utilize either the circulation control or upper surface blowing concepts, were applied to a semispan wing-fuselage model having a supercritical airfoil section. (Author)


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    Titel :

    Low Speed Aerodynamic Characteristics of Wings of Aspect Ratios 3 and 4 Equipped with High Lift Systems


    Beteiligte:
    L. A. Trobaugh (Autor:in) / D. G. Lee (Autor:in) / M. J. Harris (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    93 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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