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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    Title :

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


    Contributors:
    D. R. Riley (author)

    Publication date :

    1985


    Size :

    86 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English