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    Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear by F. Caputo, A. De Luca, A. Greco, A. Marro, A. Apicella, R. Sepe, E. Armentani

    Published 2018-01-01
    “…Usually during the design of landing gear, simplified Finite Element (FE) models, based on one-dimensional finite elements (stick model), are used to investigate the in-service reaction forces involving each subcomponent. …”
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