Deformation behaviors of defective aluminum honeycomb sandwich panels subjected to in-panel compressive loading: An experimental study with mirror-assisted multi-view DIC.

• The deformation behaviors of aluminum honeycomb sandwich panels with artificial defects of different sizes under in-panel compression were investigated using mirror-assisted MV-DIC. • Dual-surface in-plane deformation fields and through-thickness strain fields were measured. • The honeycomb sandwich panel exhibits local undulations and strain concentrations in the surface with defects. • Only defects with sufficiently large sizes leads to decreases in the buckling load. • The bending direction of the buckled specimen is influenced by the local undulations caused by the defect. Honeycomb sandwich panels have been extensively utilized in the aerospace and automotive industries for their prominent advantages of energy absorption, high strength and tailorable anisotropic mechanical properties. Nevertheless, the common presence of local core-to-skin disbonding poses an urgent need to understand the mechanical behaviors of defective honeycomb sandwich panels. The present work investigates the deformation behaviors and evolutions of aluminum honeycomb sandwich panels with varying sizes of circular artificial core-to-skin disbonding defects using mirror-assisted multi-view digital image correlation (MV-DIC). Based on the 3D profiles and dual-surface deformation fields obtained with mirror-assisted MV-DIC, it is revealed that disbonding defects induced local surface undulations with severe local strain concentrations and determined the mode of gradual bending and buckling. Defects with a diameter below 20 mm induced minor local surface undulations and slight decreases in buckling load. When the diameters of defects reach 30 mm, extensive surface convex deformation occurs and the buckling load decreases by 23 %. The results validate mirror-assisted MV-DIC as a cost-effective and practical technique for characterizing dual-surface 3D deformation of sheet composite materials and structures. [ABSTRACT FROM AUTHOR]