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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft


    Contributors:

    Conference:

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


    Publication date :

    2016-01-04


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft

    Nguyen, Nhan T. / Ting, Eric / Lebofsky, Sonia | AIAA | 2016



    Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft (AIAA 2016-1094)

    Nguyen, Nhan T. / Ting, Eric / Lebofsky, Sonia | British Library Conference Proceedings | 2016



    Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft

    Su, W. / Cesnik, C. | British Library Conference Proceedings | 2009