2007
DOI: 10.1016/j.compositesa.2006.10.007
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Simulation of progressive damage development in braided composite tubes under axial compression

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Cited by 99 publications
(51 citation statements)
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“…The method has the potential to be combined with other in-plane damage theories (e.g. continuum damage models developed at the UBC Composites Group [27,26,12]), where intra-laminar damage is treated in a smeared manner, and the element stiffness is reduced gradually as a function of damage evolution within the finite element volume. Such methodology combines the numerical advantages of smeared modelling techniques with the need to model delamination in a discrete manner.…”
Section: Discussionmentioning
confidence: 99%
“…The method has the potential to be combined with other in-plane damage theories (e.g. continuum damage models developed at the UBC Composites Group [27,26,12]), where intra-laminar damage is treated in a smeared manner, and the element stiffness is reduced gradually as a function of damage evolution within the finite element volume. Such methodology combines the numerical advantages of smeared modelling techniques with the need to model delamination in a discrete manner.…”
Section: Discussionmentioning
confidence: 99%
“…The simulated force‐displacement curve and damage failure morphology well agree with test results. McGregor et al predicted the energy‐absorption capacity of a braided composite square tube based on the continuum damage mechanics (CDMs) material model, and the numerical simulation results well agree with test results. However, their calculation results are more sensitive to the friction coefficient, fracture energy, and trigger mechanism setting.…”
Section: Introductionmentioning
confidence: 87%
“…Parametric studies were conducted to examine the effects of the tube ' s length, thickness, type of braid, and the loading conditions on the crushing behavior of tubes. Meanwhile, McGregor et al [8] studied the damage propagation, failure morphology, and energy absorption of braided composite tubes under axial compression.…”
Section: Introductionmentioning
confidence: 99%