A six-degree-of-freedom nonlinear simulation was developed for a two-place, single-engine, low-wing general aviation airplane for the stall and initial departure regions of flight. Two configurations, one with and one without an outboard wing-leading-edge modification, were modeled. The math models developed are presented simulation predictions and flight-test data for validation purposes and simulation results for the two configurations for various maneuvers and power settings are compared to show the beneficial influence of adding the wing-leading-edge modification.


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    Titel :

    Simulator Study of the Stall Departure Characteristics of a Light General Aviation Airplane with and Without a Wing-Leading-Edge Modification


    Beteiligte:
    D. R. Riley (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    86 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch