The purpose was to develop a bank of aerodynamic data including high angle-of-attack aerodynamic characteristics of 2-D airfoils and characteristics of 3-D wings and of complete airplanes beyond the stall. To fill gaps in available literature, flow visualization studies and wind tunnel tests were to be conducted. Also, a flow visualization laboratory was to be established to study wing stall and anti-stall devices. The flow visualization laboratory is in operation. A bank of 2-D high angle-of-attack airfoil data was compiled. The 3-D data were acquired; water tunnel and wind tunnel reflection plane tests were performed and continue. Data obtained indicated that movable leading-edge control surfaces show promise toward the goal of controlled flight beyond the stall.


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    Titel :

    Stall/Spin Aerodynamic Data Project


    Beteiligte:
    M. H. Snyder (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    123 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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