S´ergio Costa, Hana Zrida, Miguel Herraez, Robin Olsson, Rickard ¨Ostlund
{"title":"使用基于物理的有限变形模型模拟损伤增长","authors":"S´ergio Costa, Hana Zrida, Miguel Herraez, Robin Olsson, Rickard ¨Ostlund","doi":"10.23967/composites.2021.073","DOIUrl":null,"url":null,"abstract":"A mesoscale model for fibre kinking [2] is merged with a model for matrix fracture [1]. The fibre kinking behaviour is based on fibre kinking theory and finite deformation. The nonlin-ear behaviour is pressure dependent and is modelled by combining damage and friction on the fracture plane. The damage and fibre rotation due to kinking growth affects the transverse behaviour and vice-versa. The model shows efficiency considering the high complexity mech-anisms involved. For verification the model is tested against micro-mechanical FE simulations with multi-axial stress states such as σ 22 − σ 11 and τ 12 − σ 11 and against selected component tests. The combination of both models results in a high definition and physically-based 3D constitutive model for damage growth and crash of composite materials.","PeriodicalId":392595,"journal":{"name":"VIII Conference on Mechanical Response of Composites","volume":"634 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Modelling Damage Growth Using a Physically-Based and Finite Deformation Model\",\"authors\":\"S´ergio Costa, Hana Zrida, Miguel Herraez, Robin Olsson, Rickard ¨Ostlund\",\"doi\":\"10.23967/composites.2021.073\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A mesoscale model for fibre kinking [2] is merged with a model for matrix fracture [1]. The fibre kinking behaviour is based on fibre kinking theory and finite deformation. The nonlin-ear behaviour is pressure dependent and is modelled by combining damage and friction on the fracture plane. The damage and fibre rotation due to kinking growth affects the transverse behaviour and vice-versa. The model shows efficiency considering the high complexity mech-anisms involved. For verification the model is tested against micro-mechanical FE simulations with multi-axial stress states such as σ 22 − σ 11 and τ 12 − σ 11 and against selected component tests. The combination of both models results in a high definition and physically-based 3D constitutive model for damage growth and crash of composite materials.\",\"PeriodicalId\":392595,\"journal\":{\"name\":\"VIII Conference on Mechanical Response of Composites\",\"volume\":\"634 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"VIII Conference on Mechanical Response of Composites\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23967/composites.2021.073\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"VIII Conference on Mechanical Response of Composites","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23967/composites.2021.073","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Modelling Damage Growth Using a Physically-Based and Finite Deformation Model
A mesoscale model for fibre kinking [2] is merged with a model for matrix fracture [1]. The fibre kinking behaviour is based on fibre kinking theory and finite deformation. The nonlin-ear behaviour is pressure dependent and is modelled by combining damage and friction on the fracture plane. The damage and fibre rotation due to kinking growth affects the transverse behaviour and vice-versa. The model shows efficiency considering the high complexity mech-anisms involved. For verification the model is tested against micro-mechanical FE simulations with multi-axial stress states such as σ 22 − σ 11 and τ 12 − σ 11 and against selected component tests. The combination of both models results in a high definition and physically-based 3D constitutive model for damage growth and crash of composite materials.