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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    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


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 63 , 2 ; 357-361


    Publication date :

    2020-04-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Static Analysis of Sandwich Panels with Square Honeycomb Core

    Kapania, Rakesh K. / Soliman, Hazem E. / Vasudeva, Summit et al. | AIAA | 2008


    On the Static Analysis of Sandwich Panels with Square Honeycomb Core

    Soliman, Hazem / Makhecha, Dhaval / Vasudeva, Sumit et al. | AIAA | 2006


    Failure of Alternate Honeycomb Core Sandwich Panels

    Shah, Udit / Kapania, Rakesh K. | AIAA | 2019


    Compression After Impact Analysis on Thin Face Sheet Honeycomb Core Sandwich Panels

    McQuigg, Thomas D. / Kapania, Rakesh K. / Scotti, Stephen J. et al. | AIAA | 2013