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Buckling and post-buckling analysis of auxetic cellular structures

Communication avec acte
Auteur
ccBELHADJAMOR, Meriem
450279 Laboratoire de Génie Mécanique [Monastir] [LGM / ENIM]
ccBEN BETTAIEB, Mohamed
178323 Laboratoire d'Etude des Microstructures et de Mécanique des Matériaux [LEM3]
243747 Labex DAMAS
ccMEZLINI, Salah
558936 Ecole Nationale d’Ingénieurs de Carthage [ENICARTHAGE]
ccABED-MERAIM, Farid
178323 Laboratoire d'Etude des Microstructures et de Mécanique des Matériaux [LEM3]
243747 Labex DAMAS

URI
http://hdl.handle.net/10985/26506
Date
2024-07

Résumé

Numerical simulations and experimental tests are performed in this contribution to investigate buckling and failure modes of auxetic cellular structures as well as sandwich panels with auxetic cores. Various Poison’s ratios and densities are employed to assess their effects on the deformation mechanisms under uniaxial compression. The numerical simulations are achieved using the Riks method while accounting for geometric nonlinearity and plasticity. The results reveal that negative Poison’s ratio and structure density have significant effects on buckling critical stress and failure mechanisms of cellular structures. While the inversed honeycomb and the double arrowhead with different Poisson’s ratios display similar load capacity, the facesheet failure is more marked with the conventional inversed honeycomb. This outcome is due to the dominant effect of the facesheet on the load evolution. The impact of cell-wall thickness and facesheet thickness on the buckling load is discussed based on the FE model.

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  • Numerical Investigation on the Inelastic Instability of Cruciform Columns: Effect of Material and Geometric Parameters 
    Chapitre d'ouvrage scientifique
    BELHADJAMOR, Meriem; ccBEN BETTAIEB, Mohamed; MEZLINI, Salah; ccABED-MERAIM, Farid  (Springer Nature Switzerland, 2024-08)
    This work deals with a numerical investigation of the onset of inelastic instability in cruciform columns using the limit-point method. In this aim, a nonlinear buckling analysis was developed to determine the limit-point ...
  • Development and implementation of a new computational strategy for the prediction of elastoplastic buckling 
    Article dans une revue avec comité de lecture
    BEL HADJ AMOR, M.; ccBEN BETTAIEB, Mohamed; MEZLINI, S.; ccABED-MERAIM, Farid  (World Scientific Pub Co Pte Ltd, 2024-07)
    This study proposes an innovative computational strategy to predict the initiation of elastoplastic buckling in shell structures. This strategy is developed in connection with ABAQUS/Standard Finite Element (FE) code. ...
  • Buckling and post-buckling behavior of auxetic cellular structures 
    Article dans une revue avec comité de lecture
    BELHADJAMOR, M; BELGHITH, S; ccBEN BETTAIEB, Mohamed; MEZLINI, S; ccABED-MERAIM, Farid  (SAGE Publications, 2024-12)
    In this work, experimental tests and numerical simulations are carried out to investigate the buckling behavior and failure modes of auxetic cellular structures and sandwich panels with auxetic cores. Different Poisson's ...
  • An anisotropic model with linear perturbation technique to predict HCP sheet metal ductility limit 
    Communication avec acte
    JEDIDI, Mohamed Yassine; ccBEN BETTAIEB, Mohamed; ccABED-MERAIM, Farid ; KHABOU, Mohamed Taoufik; BOUGUECHA, Anas; HADDAR, Mohamed (2021)
    In this paper, hexagonal closed packed (HCP) sheet metal ductility for a viscoplastic material is analyzed by using a linear perturbation technique. It can be used for the analysis of localized necking. This technique is ...
  • Prediction of necking in HCP sheet metals using a two-surface plasticity model 
    Article dans une revue avec comité de lecture
    JEDIDI, Mohamed Yassine; ccBEN BETTAIEB, Mohamed; ccABED-MERAIM, Farid ; KHABOU, Mohamed Taoufik; BOUGUECHA, Anas; HADDAR, Mohamed (Elsevier, 2020)
    In the present contribution, a two-surface plasticity model is coupled with several diffuse and localized necking criteria to predict the ductility limits of hexagonal closed packed sheet metals. The plastic strain is ...

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