This paper investigates the inertial force effect on nonlinear aeroelasticity of flexible wing aircraft. The geometric are nonlinearity due to rotational and tension stiffening. The effect of large bending deflection will also be investigated. Flutter analysis will be conducted for a truss-braced wing aircraft concept with tension stiffening and inertial force coupling.


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    Titel :

    Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft


    Beteiligte:
    Nguyen, Nhan T. (Autor:in) / Ting, Eric (Autor:in)

    Kongress:

    AIAA SciTech 2016 ; 2016 ; San Diego, CA, United States


    Erscheinungsdatum :

    2016-01-04


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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