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This document investigates the bending behavior of aluminum alloy honeycomb sandwich structures through four-point bending tests. Four specimens with varying core thicknesses (10mm, 14mm) and skin thicknesses (0.5mm, 0.75mm) were tested. The results show that the honeycomb panels demonstrate initial linear elastic behavior followed by nonlinear elastic-plastic behavior under loading. Failure modes are also reported and discussed. Finite element analysis was used to model and analyze the flexural behavior of

Author

Gracie Ortega

Language

EN