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An integrated methodology and formulations for micro/macro modeling and analysis of metal matrix composites.

机译:用于金属基复合材料的微观/宏观建模和分析的集成方法和公式。

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摘要

Composites are attractive for engineering applications due to their light weight and high strength. Of the various types of composites, Metal Matrix Composites (MMC) are of interest here because of their ability to withstand very high temperatures. Hence, these composites are an excellent candidate for aircraft and aerospace structural components where elevated temperatures are frequently encountered. Routine testing/analysis of complex composite geometries such as those encountered in aircraft structures are cost-prohibitive and/or impractical, especially in hostile temperature environments. Therefore, there is a need for the development of effective computational methods and modeling/analysis techniques involving linear/nonlinear material behavior for analyzing such structural geometries.; An integrated micro/macromechanics procedure for the stress analysis of unidirectional MMC's is proposed. The micromechanical analysis is used to obtain the effective elastic moduli via the Composite Cylinder Assemblage model (CCA) or the Representative Unit Cell approach (RUC). On the other hand, for the macroscopic analysis, the macromechanical stress-strain relation is based on a modification of the so-called Vanishing Fiber Diameter theory (VFD). The fibers are considered to be linear elastic. The matrix viscoplastic behavior is described by either the Bodner and Partom or the Power Law models. The proposed integrated methodology allows the use of: (i) a physically realistic constitutive model; (ii) a macromechanical stress-strain formulation via the VFD theory; (iii) an elastic-viscoplastic constitutive material behavior; (iv) a smeared finite element procedure; and (v) efficient numerical algorithms for analyzing the behavior of composite structures. The proposed developments are validated with available experimental and analytical results for simple geometries whenever feasible, and an application to a realistic practical problem is also demonstrated.
机译:复合材料重量轻,强度高,因此在工程应用中具有吸引力。在各种类型的复合材料中,金属基复合材料(MMC)在这里很受关注,因为它们能够承受很高的温度。因此,这些复合材料是经常遇到高温的飞机和航空航天结构部件的理想选择。对复杂的复合材料几何形状(例如飞机结构中遇到的几何形状)进行例行测试/分析是成本过高和/或不切实际的,尤其是在恶劣的温度环境中。因此,需要开发包括线性/非线性材料行为的有效计算方法和建模/分析技术,以分析这种结构几何形状。提出了一种用于单向MMC应力分析的集成微观/宏观力学程序。微机械分析用于通过复合圆柱体装配模型(CCA)或典型单位单元方法(RUC)获得有效的弹性模量。另一方面,对于宏观分析,宏观机械应力-应变关系是基于对所谓的消失纤维直径理论(VFD)的修改。纤维被认为是线性弹性的。基质粘塑性行为由Bodner和Partom或幂定律模型描述。拟议的综合方法允许使用:(i)物理上现实的本构模型; (ii)通过VFD理论得出的宏观机械应力-应变公式; (iii)弹性-粘塑性本构材料的行为; (iv)涂抹有限元程序; (v)用于分析复合结构行为的有效数值算法。在可行的情况下,对于简单的几何图形,可用可用的实验和分析结果对提出的开发进行了验证,并且还演示了对实际问题的应用。

著录项

  • 作者

    Avila, Antonio Ferreira.;

  • 作者单位

    University of Minnesota.;

  • 授予单位 University of Minnesota.;
  • 学科 Engineering Mechanical.; Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 184 p.
  • 总页数 184
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;工程材料学;
  • 关键词

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