The crushing response of polycarbonate circular cell honeycomb to inplane uniaxial loading under displacement control is analyzed through a combination of experiment and numerical simulation. The experiments, which correspond to two different uniaxial loading conditions, are performed using honeycomb material which has a nearly periodic microstructure. In the initial part of the response, the specimens deform in a uniform fashion. Next, a nonlinear phase characterized by progressive localization of deformation is observed. The progressive localization causes the walls of each cell to contact. These experimental results are simulated through numerical analysis using the finite element method. The reasons for the orthotropic response of the honeycombs are discussed.
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e-mail: chungae@engin.umich.edu
e-mail: dcw@engin.umich.edu
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October 1999
Technical Papers
Compressive Response and Failure of Circular Cell Polycarbonate Honeycombs Under Inplane Uniaxial Stresses
Jaeung Chung,
Jaeung Chung
Department of Aerospace Engineering, The University of Michigan, Ann Arbor, Ml 48109-2140
e-mail: chungae@engin.umich.edu
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Anthony M. Waas
Anthony M. Waas
Department of Aerospace Engineering, The University of Michigan, Ann Arbor, Ml 48109-2140
e-mail: dcw@engin.umich.edu
Search for other works by this author on:
Jaeung Chung
Department of Aerospace Engineering, The University of Michigan, Ann Arbor, Ml 48109-2140
e-mail: chungae@engin.umich.edu
Anthony M. Waas
Department of Aerospace Engineering, The University of Michigan, Ann Arbor, Ml 48109-2140
e-mail: dcw@engin.umich.edu
J. Eng. Mater. Technol. Oct 1999, 121(4): 494-502 (9 pages)
Published Online: October 1, 1999
Article history
Received:
December 21, 1998
Revised:
May 5, 1999
Online:
November 27, 2007
Citation
Chung, J., and Waas, A. M. (October 1, 1999). "Compressive Response and Failure of Circular Cell Polycarbonate Honeycombs Under Inplane Uniaxial Stresses." ASME. J. Eng. Mater. Technol. October 1999; 121(4): 494–502. https://doi.org/10.1115/1.2812407
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