This paper presented methods to determine the aerodynamic forces that act on an aircraft wing during flight. These methods are initially proposed for a simplified two degree-of-freedoms airfoil model and then are extensively applied for a multi-degree-of-freedom airfoil system. Different airspeed conditions are considered in establishing such methods. The accuracy of the presented methods is verified by comparing the estimated aerodynamic forces with the actual values. A good agreement is achieved through the comparisons and it is verified that the present methods can be used to correctly identify the aerodynamic forces acting on the aircraft wing models.


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    Titel :

    Analytical Methods of Evaluating Aerodynamic Forces of Aircraft Wings


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Bi, Xueguang (Autor:in) / Liu, Yucheng (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 2009



    Erscheinungsdatum :

    10.11.2009




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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