{"title":"编织纺织复合材料的压缩不稳定性","authors":"Shu Ching Quek, A. Waas, V. Agaram, K. Shahwan","doi":"10.1115/imece2001/ad-25306","DOIUrl":null,"url":null,"abstract":"\n This paper discusses the results of a finite element (FE) based study of the compressive instabilities of braided glass fiber composites. The micromodel was based on a 2-unitcell size 3-D FE model. Computational tests were carried out to first determine the elastic moduli of the system. Once the computational model was validated with experimental data for the elastic moduli, the compressive response of the micromodel was established using the RIKS method option available in the ABAQUS commercial FE code. The present approach is different from that reported in the literature where classical methods based on the technique of homogenization is used to model the elastic and inelastic response of braided composites. In the present work, explicit account of the braid microstructure (geometry and packing) and the inelastic properties of the matrix are accounted for via the use of the FE method. The macromechanical data pertaining to the braided composites were obtained through traditional means. Tensile tests were performed on the composites through the usage of ASTM D 3039 standard to obtain the macroscopic orthotropic moduli and response. For each test, 3 samples were used to ensure accuracy and the average data is reported in this paper. A separate test was conducted to obtain the in-situ matrix properties of the glass braided composites. The computational model provides a means to assess the compressive strength of braided composites and its dependence on various microstructural parameters. It also serves as a tool to assess the most significant parameter that affects compressive strength. Furthermore, the model is useful to understand the response of braided composites under multiaxial loads.","PeriodicalId":442756,"journal":{"name":"Damage Initiation and Prediction in Composites, Sandwich Structures and Thermal Barrier Coatings","volume":"19 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2001-11-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Compressive Instabilities in Braided Textile Composites\",\"authors\":\"Shu Ching Quek, A. Waas, V. Agaram, K. Shahwan\",\"doi\":\"10.1115/imece2001/ad-25306\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"\\n This paper discusses the results of a finite element (FE) based study of the compressive instabilities of braided glass fiber composites. The micromodel was based on a 2-unitcell size 3-D FE model. Computational tests were carried out to first determine the elastic moduli of the system. Once the computational model was validated with experimental data for the elastic moduli, the compressive response of the micromodel was established using the RIKS method option available in the ABAQUS commercial FE code. The present approach is different from that reported in the literature where classical methods based on the technique of homogenization is used to model the elastic and inelastic response of braided composites. In the present work, explicit account of the braid microstructure (geometry and packing) and the inelastic properties of the matrix are accounted for via the use of the FE method. The macromechanical data pertaining to the braided composites were obtained through traditional means. Tensile tests were performed on the composites through the usage of ASTM D 3039 standard to obtain the macroscopic orthotropic moduli and response. For each test, 3 samples were used to ensure accuracy and the average data is reported in this paper. A separate test was conducted to obtain the in-situ matrix properties of the glass braided composites. The computational model provides a means to assess the compressive strength of braided composites and its dependence on various microstructural parameters. It also serves as a tool to assess the most significant parameter that affects compressive strength. 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引用次数: 0
摘要
本文讨论了基于有限元法研究编织玻璃纤维复合材料压缩不稳定性的结果。微观模型基于2单元尺寸的三维有限元模型。首先进行了计算试验,确定了系统的弹性模量。一旦计算模型与弹性模量的实验数据进行验证,使用ABAQUS商用有限元代码中的RIKS方法选项建立微观模型的压缩响应。本文的方法不同于文献报道的基于均匀化技术的经典方法来模拟编织复合材料的弹性和非弹性响应。在本工作中,明确说明编织的微观结构(几何形状和填料)和非弹性性质的矩阵是通过使用有限元方法。编织复合材料的宏观力学数据是通过传统方法获得的。采用ASTM D 3039标准对复合材料进行拉伸试验,得到其宏观正交各向异性模量和响应。为保证准确性,每次测试使用3个样本,文中取平均值。另外进行了原位基体性能测试。该计算模型提供了一种方法来评估编织复合材料的抗压强度及其对各种微观结构参数的依赖。它还可以作为评估影响抗压强度的最重要参数的工具。此外,该模型有助于理解编织复合材料在多轴载荷作用下的响应。
Compressive Instabilities in Braided Textile Composites
This paper discusses the results of a finite element (FE) based study of the compressive instabilities of braided glass fiber composites. The micromodel was based on a 2-unitcell size 3-D FE model. Computational tests were carried out to first determine the elastic moduli of the system. Once the computational model was validated with experimental data for the elastic moduli, the compressive response of the micromodel was established using the RIKS method option available in the ABAQUS commercial FE code. The present approach is different from that reported in the literature where classical methods based on the technique of homogenization is used to model the elastic and inelastic response of braided composites. In the present work, explicit account of the braid microstructure (geometry and packing) and the inelastic properties of the matrix are accounted for via the use of the FE method. The macromechanical data pertaining to the braided composites were obtained through traditional means. Tensile tests were performed on the composites through the usage of ASTM D 3039 standard to obtain the macroscopic orthotropic moduli and response. For each test, 3 samples were used to ensure accuracy and the average data is reported in this paper. A separate test was conducted to obtain the in-situ matrix properties of the glass braided composites. The computational model provides a means to assess the compressive strength of braided composites and its dependence on various microstructural parameters. It also serves as a tool to assess the most significant parameter that affects compressive strength. Furthermore, the model is useful to understand the response of braided composites under multiaxial loads.