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    Title :

    Static Aeroelastic and Longitudinal Trim Model of Flexible Wing Aircraft Using Finite-Element Vortex-Lattice Coupled Solution (AIAA 2014-0837)



    Conference:

    Conference; 55th, AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials ; 2014 ; National Harbor, MD



    Publication date :

    2014-01-01


    Size :

    29 pages


    Remarks:

    Includes bibliographical references and author index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






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