期刊
JOURNAL OF SANDWICH STRUCTURES & MATERIALS
卷 14, 期 6, 页码 679-693出版社
SAGE PUBLICATIONS LTD
DOI: 10.1177/1099636212460537
关键词
Cohesive zone modeling; debond; buckling-induced debond growth; honeycomb sandwich panel; double cantilever beam test
Buckling-induced skin-core debond growth in honeycomb sandwich cantilever beam is demonstrated using a cohesive zone model. The input parameters for the analysis are interfacial bond strength, mode I and mode II interfacial fracture toughness values, obtained from flatwise tension tests, drum-peel tests and three-point end notch flexure tests, respectively. Debonded honeycomb specimens are tested and the acoustic emission technique was used to observe the initiation of the debond growth. The load-displacement response from the cohesive zone model model shows a good agreement with the experimental results. The conventional analysis without cohesive zone model overestimates failure load by 56%. Cohesive zone model is able to predict the coupled debond growth and buckling failure in honeycomb sandwich structures.
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