Composite Beam Cross-Section Analysis by a Single High-Order Element Layer

Philippe Couturier, Steen Krenk

    Research output: Chapter in Book/Report/Conference proceedingArticle in proceedingsResearchpeer-review

    Abstract

    An analysis procedure of general cross-section properties is presented. The formulation is based on the stress-strain states in the classic six equilibrium modes of a beam by considering a finite thickness slice modelled by a single layer of 3D finite elements. The theory is illustrated by application to composite sections of various shapes and material layups.
    Original languageEnglish
    Title of host publicationProceedings of 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
    Number of pages9
    PublisherAmerican Institute of Aeronautics and Astronautics
    Publication date2015
    DOIs
    Publication statusPublished - 2015
    Event56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference - Gaylord Palms and Convention Center, Kissimmee, United States
    Duration: 5 Jan 20159 Jan 2015

    Conference

    Conference56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
    LocationGaylord Palms and Convention Center
    Country/TerritoryUnited States
    CityKissimmee
    Period05/01/201509/01/2015

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