Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    AIAA-2001-1579 Deforming Mesh for Computational Aeroelasticity Using a Nonlinear Elastic Boundary Element Method



    Conference:

    42nd, Structures, structural dynamics, and materials conference ; 2001 ; Seattle, WA



    Publication date :

    2001-01-01


    Size :

    11 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







    Nonlinear Computational Aeroelasticity Using Structural Modal Coordinates (AIAA 2018-1447)

    Medeiros, Renato / Cesnik, Carlos E. / Coetzee, Etienne | British Library Conference Proceedings | 2018


    AIAA 2001-0569 Evaluation of Computational Aeroelasticity Codes for Loads and Flutter

    Huttsell, L. / Schuster, D. / Volk, J. et al. | British Library Conference Proceedings | 2001