In-plane compressive response of composite sandwich panels with local-tight honeycomb cores

In the present study, honeycomb cores with periodic tight zones were proposed for carbon-fiber and aluminum -honeycomb sandwich panels by flattening hexagon-shaped cells of honeycomb walls. In-plane compression tests were performed for sandwich panels with three types of local-tight honeycomb cores to evaluate the effects of the local-tight configurations on mechanical properties and failure modes. Experimental results indicated that the mechanical properties of sandwich specimens were effectively increased by using the proposed local-tight honeycomb cores. In particular, the specific energy absorption of sandwich specimens with a local -orthogonal-tight core was increased by 400.46%. In addition, Digital Image Correlation (DIC) technique was employed to further investigate the compressive behaviors of the sandwich specimens with and without local -orthogonal-tight honeycomb cores. The experimental measurements and detailed DIC observations indicated that the local-orthogonal-tight honeycomb core sandwich structures, which provided improved load transferring paths and reduced mismatch between the high-stiffness face sheets and low-stiffness core, exhibited progressive crushing failure modes.

Automated summary

In this study, honeycomb cores with periodic tight zones were proposed as structures for carbon-fiber and aluminum-honeycomb sandwich panels. In-plane compression tests were conducted to evaluate the effects of the local-tight configurations on mechanical properties and failure modes. Experimental results showed that the mechanical properties of sandwich specimens were effectively improved by using the proposed local-tight honeycomb cores. Furthermore, the use of Digital Image Correlation (DIC) technique revealed that the sandwich structures with local-orthogonal-tight honeycomb cores exhibited progressive crushing failure modes.