{"title":"玻璃钢复合材料压缩破坏的参数化高保真广义胞元法细观力学模型","authors":"I. Meshi, U. Breiman, R. Haj-Ali","doi":"10.23967/wccm-eccomas.2020.339","DOIUrl":null,"url":null,"abstract":". A multiscale model based on finite element (FE) and the Parametric High-Fidelity-Generalized-Method-of-Cells (PHFGMC) micromechanical model was formulated and implemented to solve the compression problem in unidirectional IM7/977-3 carbon epoxy composite. The nonlinear PHFGMC governing equations were obtained from a two-layered (local-global) virtual work principle and solved using a incremental-iterative formulation. In addition, the semi-analytical modified Lo and Chim failure criterion (based on the buckling of Timoshenko’s beam) for unidirectional fiber-reinforced composite materials under compression [1] was adopted and combined with the FE-PHFGMC multiscale model. In this study, the criterion was employed for the general case of a multi-axial loading state accompanied with a nonlinear polymeric matrix behavior, where the local and thus effective properties of the composite change continuously throughout the loading path. Therefore the predicted lamina strength was incrementally reevaluated. In the present model, the use of the nonlinear constitutive model Ramberg-Osgood was used for the matrix media and a linear-elastic transversely-isotropic law for the fiber, as common for carbon fibrous composites. This extends the existing criterion to account for the material microstructure with a refined parametric discretization, as well as the effect of a nonlinear constitutive law. The advantage of the proposed model is to predict the compressive damage (kink band formation and its width) and the compressive strength (within 11% of experimental data)","PeriodicalId":148883,"journal":{"name":"14th WCCM-ECCOMAS Congress","volume":"21 6","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"The Parametric High-Fidelity-Generalized-Method-of-Cells (PHFGMC) Micromechanical Model for Compression Failure of FRP Composites\",\"authors\":\"I. Meshi, U. Breiman, R. Haj-Ali\",\"doi\":\"10.23967/wccm-eccomas.2020.339\",\"DOIUrl\":null,\"url\":null,\"abstract\":\". A multiscale model based on finite element (FE) and the Parametric High-Fidelity-Generalized-Method-of-Cells (PHFGMC) micromechanical model was formulated and implemented to solve the compression problem in unidirectional IM7/977-3 carbon epoxy composite. The nonlinear PHFGMC governing equations were obtained from a two-layered (local-global) virtual work principle and solved using a incremental-iterative formulation. In addition, the semi-analytical modified Lo and Chim failure criterion (based on the buckling of Timoshenko’s beam) for unidirectional fiber-reinforced composite materials under compression [1] was adopted and combined with the FE-PHFGMC multiscale model. In this study, the criterion was employed for the general case of a multi-axial loading state accompanied with a nonlinear polymeric matrix behavior, where the local and thus effective properties of the composite change continuously throughout the loading path. Therefore the predicted lamina strength was incrementally reevaluated. In the present model, the use of the nonlinear constitutive model Ramberg-Osgood was used for the matrix media and a linear-elastic transversely-isotropic law for the fiber, as common for carbon fibrous composites. This extends the existing criterion to account for the material microstructure with a refined parametric discretization, as well as the effect of a nonlinear constitutive law. The advantage of the proposed model is to predict the compressive damage (kink band formation and its width) and the compressive strength (within 11% of experimental data)\",\"PeriodicalId\":148883,\"journal\":{\"name\":\"14th WCCM-ECCOMAS Congress\",\"volume\":\"21 6\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"14th WCCM-ECCOMAS Congress\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23967/wccm-eccomas.2020.339\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"14th WCCM-ECCOMAS Congress","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23967/wccm-eccomas.2020.339","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
摘要
. 为解决单向IM7/977-3碳环氧复合材料的压缩问题,建立并实现了基于有限元(FE)和参数化高保真广义单元法(PHFGMC)的多尺度模型。利用两层(局部-全局)虚功原理得到非线性PHFGMC控制方程,并采用增量迭代法求解。采用基于Timoshenko梁屈曲的单向纤维增强复合材料半解析修正Lo and Chim破坏准则[1],并与FE-PHFGMC多尺度模型相结合。在本研究中,该准则适用于伴随非线性聚合物基体行为的多轴加载状态的一般情况,其中复合材料的局部和有效性能在整个加载路径中连续变化。因此,对预测的层板强度进行增量重新评估。在本模型中,基体介质采用非线性本构模型Ramberg-Osgood,纤维采用线弹性横向各向同性定律,与碳纤维复合材料一样。这扩展了现有的标准,以考虑材料微观结构与细化参数离散化,以及非线性本构律的影响。该模型的优点是可以预测材料的抗压损伤(扭结带的形成及其宽度)和抗压强度(在实验数据的11%以内)。
The Parametric High-Fidelity-Generalized-Method-of-Cells (PHFGMC) Micromechanical Model for Compression Failure of FRP Composites
. A multiscale model based on finite element (FE) and the Parametric High-Fidelity-Generalized-Method-of-Cells (PHFGMC) micromechanical model was formulated and implemented to solve the compression problem in unidirectional IM7/977-3 carbon epoxy composite. The nonlinear PHFGMC governing equations were obtained from a two-layered (local-global) virtual work principle and solved using a incremental-iterative formulation. In addition, the semi-analytical modified Lo and Chim failure criterion (based on the buckling of Timoshenko’s beam) for unidirectional fiber-reinforced composite materials under compression [1] was adopted and combined with the FE-PHFGMC multiscale model. In this study, the criterion was employed for the general case of a multi-axial loading state accompanied with a nonlinear polymeric matrix behavior, where the local and thus effective properties of the composite change continuously throughout the loading path. Therefore the predicted lamina strength was incrementally reevaluated. In the present model, the use of the nonlinear constitutive model Ramberg-Osgood was used for the matrix media and a linear-elastic transversely-isotropic law for the fiber, as common for carbon fibrous composites. This extends the existing criterion to account for the material microstructure with a refined parametric discretization, as well as the effect of a nonlinear constitutive law. The advantage of the proposed model is to predict the compressive damage (kink band formation and its width) and the compressive strength (within 11% of experimental data)