Advances in aircraft and spacecraft science

  • 제6권4호
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  • Pages.315-331
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  • 2019
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  • 2287-528X(pISSN)
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  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
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Hygrothermal effect on the moisture absorption in composite laminates with transverse cracks and delamination

  • Kesba, Mohamed Khodjet (Laboratoire des Sciences Aeronautiques, Institut d'Aeronautique et des etudes Spatiales, Universite de Blida1) ;
  • Benkhedda, A. (Laboratoire des Sciences Aeronautiques, Institut d'Aeronautique et des etudes Spatiales, Universite de Blida1) ;
  • Adda bedia, E.A. (Laboratoire des Materiaux et Hydrologie, Universite de Sidi Bel Abbes) ;
  • Boukert, B. (Laboratoire des Sciences Aeronautiques, Institut d'Aeronautique et des etudes Spatiales, Universite de Blida1)
  • 투고 : 2018.04.07
  • 심사 : 2019.03.15
  • 발행 : 2019.07.25
⟨ 이전 논문 다음 논문 ⟩

초록

The stiffness degradation of the cross-ply composite laminates containing a transverse cracking and delamination in $90^{\circ}$ layer is predicted by using a modified shear-lag model by introducing the stress perturbation function. The prediction shows better agreement with the experimental results published by Ogihara and Takeda 1995, especially for laminates with thicker $90^{\circ}$ plies in which extensive delamination occurs. A homogenised analytic model for average transient moisture uptake in composite laminates containing periodically distributed matrix cracks and delamination is presented. It is shown that the model well describes the moisture absorption in a cross-ply composite laminate containing periodically distributed transverse matrix cracks in the $90^{\circ}$ plies. The obtained results represent well the dependence of the stiffness degradation on the crack density, thickness ratio and moisture absorption. The present study has proved to be important to the understanding of the degradation of the material propertiesin the failure process when the laminates in which the delamination grows extensively.

키워드

참고문헌

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