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    New Numerical Modeling for Impact Dynamics Behavior of Composite Honeycomb Sandwich Structures

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 004
    Author:
    Muhammad Kamran
    ,
    Fan Wu
    ,
    Pu Xue
    ,
    Rong Min
    DOI: 10.1061/(ASCE)AS.1943-5525.0001129
    Publisher: ASCE
    Abstract: In the applications of composite honeycomb sandwich structures, they often are severely impacted, resulting in partial penetration or complete perforation. To study the mechanical response of composite honeycomb sandwich structures under high-velocity impact, an extended P-α model was developed to describe the equivalent property of honeycomb materials. Extended P-α model parameters were determined using analytical and experimental techniques. Based on the equivalent model, the impact response had good agreement between the experimental results and numerical simulation. By comparison with the detailed model in terms of ballistic limit, residual velocity, maximum displacement of the projectile, and contact time, the results from the equivalent model are not only reliable but also computationally efficient, because the equivalent model requires only 25% as much time as the detailed model under the same conditions.
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      New Numerical Modeling for Impact Dynamics Behavior of Composite Honeycomb Sandwich Structures

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4266628
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    contributor authorMuhammad Kamran
    contributor authorFan Wu
    contributor authorPu Xue
    contributor authorRong Min
    date accessioned2022-01-30T20:10:14Z
    date available2022-01-30T20:10:14Z
    date issued2020
    identifier other%28ASCE%29AS.1943-5525.0001129.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4266628
    description abstractIn the applications of composite honeycomb sandwich structures, they often are severely impacted, resulting in partial penetration or complete perforation. To study the mechanical response of composite honeycomb sandwich structures under high-velocity impact, an extended P-α model was developed to describe the equivalent property of honeycomb materials. Extended P-α model parameters were determined using analytical and experimental techniques. Based on the equivalent model, the impact response had good agreement between the experimental results and numerical simulation. By comparison with the detailed model in terms of ballistic limit, residual velocity, maximum displacement of the projectile, and contact time, the results from the equivalent model are not only reliable but also computationally efficient, because the equivalent model requires only 25% as much time as the detailed model under the same conditions.
    publisherASCE
    titleNew Numerical Modeling for Impact Dynamics Behavior of Composite Honeycomb Sandwich Structures
    typeJournal Paper
    journal volume33
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001129
    page04020016
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 004
    contenttypeFulltext
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