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    The Damage Tolerance of a Sandwich Panel Containing a Cracked Honeycomb Core

    Source: Journal of Applied Mechanics:;2009:;volume( 076 ):;issue: 006::page 61003
    Author:
    I. Quintana Alonso
    ,
    N. A. Fleck
    DOI: 10.1115/1.2912995
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The tensile fracture strength of a sandwich panel, with a center-cracked core made from an elastic-brittle diamond-celled honeycomb, is explored by analytical models and finite element simulations. The crack is on the midplane of the core and loading is normal to the faces of the sandwich panel. Both the analytical models and finite element simulations indicate that linear elastic fracture mechanics applies when a K-field exists on a scale larger than the cell size. However, there is a regime of geometries for which no K-field exists; in this regime, the stress concentration at the crack tip is negligible and the net strength of the cracked specimen is comparable to the unnotched strength. A fracture map is developed for the sandwich panel with axes given by the sandwich geometry. The effect of a statistical variation in the cell-wall strength is explored using Weibull theory, and the consequences of a stochastic strength upon the fracture map are outlined.
    keyword(s): Brittleness , Stress , Fracture (Materials) , Engineering simulation , Fracture (Process) , Diamonds , Fracture toughness , Failure , Geometry AND Finite element analysis ,
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      The Damage Tolerance of a Sandwich Panel Containing a Cracked Honeycomb Core

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    contributor authorI. Quintana Alonso
    contributor authorN. A. Fleck
    date accessioned2017-05-09T00:31:08Z
    date available2017-05-09T00:31:08Z
    date copyrightNovember, 2009
    date issued2009
    identifier issn0021-8936
    identifier otherJAMCAV-26767#061003_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/139672
    description abstractThe tensile fracture strength of a sandwich panel, with a center-cracked core made from an elastic-brittle diamond-celled honeycomb, is explored by analytical models and finite element simulations. The crack is on the midplane of the core and loading is normal to the faces of the sandwich panel. Both the analytical models and finite element simulations indicate that linear elastic fracture mechanics applies when a K-field exists on a scale larger than the cell size. However, there is a regime of geometries for which no K-field exists; in this regime, the stress concentration at the crack tip is negligible and the net strength of the cracked specimen is comparable to the unnotched strength. A fracture map is developed for the sandwich panel with axes given by the sandwich geometry. The effect of a statistical variation in the cell-wall strength is explored using Weibull theory, and the consequences of a stochastic strength upon the fracture map are outlined.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Damage Tolerance of a Sandwich Panel Containing a Cracked Honeycomb Core
    typeJournal Paper
    journal volume76
    journal issue6
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2912995
    journal fristpage61003
    identifier eissn1528-9036
    keywordsBrittleness
    keywordsStress
    keywordsFracture (Materials)
    keywordsEngineering simulation
    keywordsFracture (Process)
    keywordsDiamonds
    keywordsFracture toughness
    keywordsFailure
    keywordsGeometry AND Finite element analysis
    treeJournal of Applied Mechanics:;2009:;volume( 076 ):;issue: 006
    contenttypeFulltext
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