Parameter studies and evaluation principles of delamination damage in laminated composites
Parameter studies and evaluation principles of delamination damage in laminated composites作者机构:School of AstronauticsBeihang UniversityBeijing 100083China Shenyang Aircraft Design and Research InstituteShenyang 110035China College of Aerospace EngineeringChongqing UniversityChongqing 400044China
出 版 物:《Chinese Journal of Aeronautics》 (中国航空学报(英文版))
年 卷 期:2021年第34卷第7期
页 面:62-72页
核心收录:
学科分类:08[工学] 0805[工学-材料科学与工程(可授工学、理学学位)] 080502[工学-材料学]
基 金:The research work is supported by the National Science Foundation of China(Nos.11572058 11772028 11872131 and U1864208)
主 题:Analytical model Composite Delamination Evaluation principles Parameter study
摘 要:Delamination represents one of the most severe failure modes in composite laminates,especially when they are subjected to uniaxial compression *** evaluation of the delamination damage has always been an essential issue of composite laminates for durability and damage tolerance in engineering *** on the most typical and representative elliptical delamination issue,an analytical model simultaneously considering the conservative buckling process and non-conservative delamination propagation process is *** computational cases considering different delamination depths,directions,aspect ratios,and areas are established,and the predicted results based on the analytical model are carefully *** of these geometrical delamination parameters on the buckling,delamination propagation,and failure behaviors of composite laminates are thoroughly analyzed,and innovative evaluation principles of the delamination damage have been *** is found that the delamination area is the key factor that truly affecting the failure behaviors of delaminated composites,and the local/global buckling and failure loads show clear linearity with the delamination area,whilst the delamination depth and direction only have slight effects.