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《Fiber Reinforced Plastics/Composites》 2019-10
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DAMAGE PREDICTION AND MODELLING COMPARISON OF CARBON FIBER-REINFORCED COMPOSITE OPEN-HOLE LAMINATES UNDER COMPRESSION

TANG Jing;CHEN Xiao;YANG Ke;Institute of Engineering Thermophysics,Chinese Academy of Sciences;University of Chinese Academy of Sciences;National R&D center of wind turbine blade;Key Laboratory of Wind Energy Utilization,Chinese Academy of Sciences;Department of Wind Energy,Technical University of Denmark;  
The finite element models of shell elements,shell-cohesive mixed elements and shell-solid mixed elements were developed in software Abaqus to model two open-hole composite laminates( OHC),i.e. flat OHC and cylindrical OHC. The universal Abaqus built-in software and proprietary user-subroutine were respectively adopted to analyze compressive damage. The buckling,intralaminar failure and delamination of both OHCs under compression were predicted by Hashin failure criteria,modified Tsai-Wu failure criteria and Quads failure criteria,then compared with experimental results. The results show that the predicted strength of cylindrical OHC is less than 7%error for proposed five models; the damage initiation around hole and loss of loading-carrying capacity can be captured by all models. The shell model solely relying on Abaqus software with built-in Hashin failure criteria can provide an effective strength assessment of cylindrical OHC,while user-subroutines with modified Tsai-Wu failure criteria can offer a more reliable alternative for flat OHC.
【Fund】: 国家自然科学基金青年科学基金项目(51405468)
【CateGory Index】: TQ327.3;TB33
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【Citations】
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【Co-citations】
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1 MA Shaohua;WANG Yonggang;HUI Li;FEI Bingqiang;College of Electromechanical Engineering,Shenyang Aerospace University;Key Laboratory of Fundamental Science for National Defense of Aeronautical Digital Manufacturing Process;;Compressing Property of Composite Laminate With Hole in Hygrothermal Environment[J];宇航材料工艺;2015-06
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