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Modelling the failure of near-edge impacted carbon fibre-reinforced composite subjected to shear loading

Identifikátory výsledku

  • Kód výsledku v IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000077" target="_blank" >RIV/00010669:_____/18:N0000077 - isvavai.cz</a>

  • Výsledek na webu

    <a href="https://iopscience.iop.org/article/10.1088/1757-899X/369/1/012035/pdf" target="_blank" >https://iopscience.iop.org/article/10.1088/1757-899X/369/1/012035/pdf</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1088/1757-899X/369/1/012035" target="_blank" >10.1088/1757-899X/369/1/012035</a>

Alternativní jazyky

  • Jazyk výsledku

    angličtina

  • Název v původním jazyce

    Modelling the failure of near-edge impacted carbon fibre-reinforced composite subjected to shear loading

  • Popis výsledku v původním jazyce

    The failure of an impacted carbon fibre-reinforced composite is analysed, where a double impact near the edge of a large centre hole and subsequent shear loading are simulated. Three levels of impact with energies of 15 J, 25 J and 50 J are investigated, along with an impact-free panel used as control. The numerical finite-element (FE) method together with cohesive zone modelling is employed. The composite material is represented by the three-dimensional ply-by-ply FE model. The numerical results of the impacts are compared with respect to the damaged areas as described in the FE model and it is found that only the 50 J impact causes the impactor to penetrate the composite. Subsequent shear loading shows two failures during loading. The first is caused by a local loss of stability in the impacted region whereas the second is a failure in the tension diagonal of the panel. The load carrying capacity, when compared to the impact-free panel, shows on average, a reduction of 37% at the first failure. The FE modelling technique utilizing the ply-by-ply 3D model and cohesive zone representing the ply interactions is successfully adopted to simulate the shear test of the near-edge impacted composite. However, the behaviour of the compression region including the impact zone does not entirely agree with that experimentally observed during the shear test. In future studies, the compressive strength and local loss of stability should be more precisely addressed.

  • Název v anglickém jazyce

    Modelling the failure of near-edge impacted carbon fibre-reinforced composite subjected to shear loading

  • Popis výsledku anglicky

    The failure of an impacted carbon fibre-reinforced composite is analysed, where a double impact near the edge of a large centre hole and subsequent shear loading are simulated. Three levels of impact with energies of 15 J, 25 J and 50 J are investigated, along with an impact-free panel used as control. The numerical finite-element (FE) method together with cohesive zone modelling is employed. The composite material is represented by the three-dimensional ply-by-ply FE model. The numerical results of the impacts are compared with respect to the damaged areas as described in the FE model and it is found that only the 50 J impact causes the impactor to penetrate the composite. Subsequent shear loading shows two failures during loading. The first is caused by a local loss of stability in the impacted region whereas the second is a failure in the tension diagonal of the panel. The load carrying capacity, when compared to the impact-free panel, shows on average, a reduction of 37% at the first failure. The FE modelling technique utilizing the ply-by-ply 3D model and cohesive zone representing the ply interactions is successfully adopted to simulate the shear test of the near-edge impacted composite. However, the behaviour of the compression region including the impact zone does not entirely agree with that experimentally observed during the shear test. In future studies, the compressive strength and local loss of stability should be more precisely addressed.

Klasifikace

  • Druh

    D - Stať ve sborníku

  • CEP obor

  • OECD FORD obor

    20304 - Aerospace engineering

Návaznosti výsledku

  • Projekt

  • Návaznosti

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Ostatní

  • Rok uplatnění

    2018

  • Kód důvěrnosti údajů

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Údaje specifické pro druh výsledku

  • Název statě ve sborníku

    IOP Conference Series: Materials Science and Engineering

  • ISBN

  • ISSN

    17578981

  • e-ISSN

  • Počet stran výsledku

    8

  • Strana od-do

    nestrankovano

  • Název nakladatele

    Institute of Physics Publishing

  • Místo vydání

    Neuveden

  • Místo konání akce

    Kitakyushu, Japonsko

  • Datum konání akce

    10. 4. 2018

  • Typ akce podle státní příslušnosti

    WRD - Celosvětová akce

  • Kód UT WoS článku

    000437169900035