Since the aerodynamic theory is nonlinear, the method requires the coupling of two iterative processes - an aerodynamic analysis and a structural analysis. A full potential analysis code, FLO22, is combined with a linear structural analysis to yield aerodynamic load distributions on and deflections of elastic wings. This method was used to analyze an aeroelastically-scaled wind tunnel model of a proposed executive-jet transport wing and an aeroelastic research wing. The results are compared with the corresponding rigid-wing analyses, and some effects of elasticity on the aerodynamic loading are noted.


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    Titel :

    Application of a transonic potential flow code to the static aeroelastic analysis of three-dimensional wings


    Beteiligte:
    Whitlow, W., Jr. (Autor:in) / Bennett, R. M. (Autor:in)

    Kongress:

    AIAA/ASME/ASCE/AHS Struct., Structural Dyn. and Mater. Conf., ; 1982 ; New Orleans, LA, United States


    Erscheinungsdatum :

    01.04.1982


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :