پديدآورندگان :
Kamareh F Department of Mechanical Engineering, Tarbiat Modares University, Tehran, 14115-111, Iran , Rahimi G.H. Department of Mechanical Engineering, Tarbiat Modares University, Tehran, 14115-111, Iran , Farrokhabadi A amin-farrokh@modares.ac.ir Department of Mechanical Engineering, Tarbiat Modares University, Tehran, 14115-111, Iran , Malekinejad H Department of Mechanical Engineering, Tarbiat Modares University, Tehran, 14115-111, Iran
كليدواژه :
Lattice Composite , Debonding , Three Point Bending , Cohesive Zone , Experiment.
چكيده فارسي :
In present study an experimental and numerical investigation has been carried out on lattice composite panels under
bending loading. To provoke the damage growth, an initial debonding has been considered for all specimens. To simulate the
interface debonding growth, an appropriate cohesive zone model is applied in the ABAQUS commercial software in the
framework of continuum damage mechanics. The obtained results reveal an acceptable agreement between the numerical and
experimental analysis.
