Sandwich panel structures are widely used in aerospace, marine, and automotive applications due to their high stiffness, high strength-to-weight ratio, good vibration damping, and thermal conductivity. The present study investigates the response of 3D printed polylactide acid (PLA) honeycomb structures when used as a crushable core with a protective metal coating in order to analyze the extent of damage and deformation of the center of the back sheet. This research is based on experimental testing and finite element simulation. The purpose of this study is to investigate the effect of three parameters of sandwich panel core, including filling density of the sacrificial core, 3D printer nozzle thickness, and the geometry of printed cells on the strength of sandwich panel under explosive loading. In this study, the effect of these three parameters is investigated at the same time, and finally, the optimal state of these three parameters that leads to the least displacement of the center of the back sheet is introduced. At first, a sandwich structure with a honeycomb core was made by a 3D printing machine, and the filling density of the core was 13 %. Then this set was subjected to explosive loading in open air with C4 explosive and the displacement of the center of the back sheet was measured. Further, considering the cost of experimental tests, the conditions of this test were simulated by the finite element code in LS-DYNA software, and the results of the displacement of the center of the back sheet were verified by experimental testing. In the following, Design-Expert software was used to check the three parameters of filling density, geometry of cells and thickness of the 3D printer nozzle at the same time. Finally, to verify the value obtained for the optimal state, the finite element simulation and experimental test were performed by placing the input parameters of the optimal state and the results were compared.
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