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      Nonlinear Modal Condensation of Large Finite Element Models: Application of Hodges’s Intrinsic Theory

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      * ,
      AIAA Journal
      American Institute of Aeronautics and Astronautics

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          Abstract

          A method to obtain geometrically nonlinear reduced-order descriptions of structures defined by a large finite element model is presented. The full model is used to identify all the coefficients in a modal projection of Hodges’s intrinsic beam equations, with the geometric reduction introduced through static or dynamic condensation along the main load paths on the original structure. The only information retrieved from the full model is the linear normal modes as well as condensed mass and stiffness and nodal coordinates. The approach aims to solve geometrically nonlinear problems of industrial complexity in an efficient manner, while preserving the linear model under small displacements. Examples of increasing complexity will be shown with the built-up finite element models made with beams and shells and both lumped and distributed masses. Nonlinear static and dynamic analyses, including rigid-body dynamics, are then demonstrated using the resulting nonlinear modal description.

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            State of the art in wind turbine aerodynamics and aeroelasticity

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              On the dynamics in space of rods undergoing large motions — A geometrically exact approach

                Author and article information

                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                18 December 2018
                October 2019
                : 57
                : 10
                : 4255-4268
                Affiliations
                Imperial College , London, England SW7 2AZ, United Kingdom
                Author notes
                [*]

                Professor of Computational Aeroelasticity, Department of Aeronautics, Room CAGB 338, South Kensington Campus; r.palacios@ 123456imperial.ac.uk . Associate Fellow AIAA.

                [†]

                Graduate Research Assistant, Department of Aeronautics, Room CAGB 309, South Kensington Campus.

                Article
                J057556 J057556
                10.2514/1.J057556
                b9a8fb76-ca68-4fdd-afde-e53afc069f6c
                Copyright © 2018 by Alvaro Cea and Rafael Palacios. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 29 May 2018
                : 27 August 2018
                : 11 October 2018
                Page count
                Figures: 19, Tables: 1
                Funding
                Funded by: Engineering and Physical Sciences Research Council10.13039/501100000266
                Award ID: N/A
                Categories
                Asymptotic Analyses, Dynamics, and Aeroelasticity

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

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