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基于Kalman滤波技术的纤维增强复合材料界面断裂参数确定方法

何周理 徐绯 段敏鸽

航空材料学报2012,Vol.32Issue(1):89-94,6.
航空材料学报2012,Vol.32Issue(1):89-94,6.DOI:10.3969/j.issn.1005-5053.2012.1.018

基于Kalman滤波技术的纤维增强复合材料界面断裂参数确定方法

Identification of Interface Fracture Parameters of Fiber-reinforced Composite by Using Kalman Filter Technology

何周理 1徐绯 2段敏鸽1

作者信息

  • 1. 西北工业大学航空学院,西安710072
  • 2. 上海飞机设计研究院,上海200232
  • 折叠

摘要

Abstract

The fiber reinforced composite has the advantages of low density, high strength and stiffness, high fatigue resistance, high abrasion and corrosion resistance, good molding and high temperature resistance, which makes it as the brightest material applied in the aerospace and aviation field. In this paper, Kalman filter technology which originally came from the field of signal control is introduced as an inverse analysis to identify the interface parameters of composites. By performing detailed FEM simulation and using the experimental data of the force and displacement curve of the fiber pull-out test, the Kalman filter recursive process is successfully carried out to identify the values of the shear strength and the fracture energy G for the SiC ( SCS-6) /Ti material interface. The great advantage of this inverse technology is that the influence of experimental noise can be taken into account. The calculation results show that the rate of convergence to the correct solution depends on the number and the initial estimation of unknown parameters to be identified and the accuracy of the measured data. Our analysis demonstrates that the proposed approach is suitable and capable in the identification of material parameters of the composite interface.

关键词

Kalman滤波/反演分析/材料界面/剪切强度/断裂能

Key words

Kalman-filter/ inverse analysis/ material interface/ shear strength/ fracture energy

分类

数理科学

引用本文复制引用

何周理,徐绯,段敏鸽..基于Kalman滤波技术的纤维增强复合材料界面断裂参数确定方法[J].航空材料学报,2012,32(1):89-94,6.

基金项目

2008年教育部新世纪优秀人才支持计划资助(NCET080454)及航空科学基金(2010ZF53071) (NCET080454)

航空材料学报

OA北大核心CSCDCSTPCD

1005-5053

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