This paper presents a simple method for structural analysis of honeycomb sa
ndwich panel (HSP), which is used as light weight and high stiffness materi
al. It is shown that the rigidity of honeycomb core is very influential to
the stiffness of HSP when HSP is subjected to bending load, and elastic and
plastic moduli of rigidity are given by honeycomb parameters such as cell
size and cell wall thickness. Therefore the authors propose the finite elem
ent model for structural analysis of HSP, which can simulate the HSP deform
ed behavior without detailed hexagonal mesh. The analyses results given by
the proposed element agree with the results of the experiment and the detai
led meshing analyses. This element doesn't reduce the precision but signifi
cantly reduces the time for pre and post processes, and analyses.