The objective of the research presented in this paper was to determine the honeycomb core compliance of a sandwich structure of the horizontal stabilizer of the MiG-29 fighter jet in the static compression test. The study of the specimen was conducted based on the ASTM C365/C365M standard. The article presents the results of experimentally determined dependencies and strength parameters, i.e. the force-displacement dependence, the compressive modulus and the honeycomb core deformations.


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    Titel :

    Examination of Honeycomb Core Compliance in Sandwich Structure


    Beteiligte:
    Nowakowski Dominik (Autor:in) / Baran Marta (Autor:in) / Lisiecki Janusz (Autor:in) / Kłysz Sylwester (Autor:in) / Synaszko Piotr (Autor:in)


    Erscheinungsdatum :

    2019




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




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