This paper presents the simulation results for the three-layered aluminum honeycomb panels with face sheets made of composite aluminum alloy filled with silicon carbide particles. The effect of the filler volume fraction on the load bearing capacity of a simply supported panel under condition of static loading with uniformly distributed pressure and under the impact over the panel surface with a rigid spherical body is investigated. It is shown that the static and dynamic characteristics of the panel change in a different way depending on the filler volume fraction.


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    Titel :

    Evaluation of the Load Bearing Capacity of the Honeycomb Core Sandwich Panels with Face Sheets Made of Metal Matrix Composite under Static and Dynamic Loading


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:
    Volkov, A. V. (Autor:in) / Solyaev, Yu. O. (Autor:in) / Rabinskii, L. N. (Autor:in) / Shavnev, A. A. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 63 , 2 ; 357-361


    Erscheinungsdatum :

    2020-04-01


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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