☆ 4.6 Article

Face/core disbond fatigue growth in honeycomb cored aircraft sandwich elements under mixed mode flatwise tension loading

JOURNAL OF SANDWICH STRUCTURES & MATERIALS (2023)

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Summary: The fracture mechanics analysis of a face/core interface crack in a honeycomb core sandwich under mode I-dominated loading conditions is conducted to examine the homogenized in-plane extensional properties. The study shows that plane stress assumption may lead to crack closure effects and highly distorted core elements for core with low in-plane modulus, while plane strain stabilizes the core deformation. Experimental results support the plane strain constrained modulus approach for face/core debond analysis.

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