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复合材料层合板低速冲击损伤影响因素分析

屈天骄 郑锡涛 范献银 郑晓霞

航空材料学报2011,Vol.31Issue(6):81-86,6.
航空材料学报2011,Vol.31Issue(6):81-86,6.DOI:10.3969/j.issn.1005-5053.2011.6.014

复合材料层合板低速冲击损伤影响因素分析

Exploration of Several Influence Factors of Low-Velocity Impact Damage on Composite Laminates

屈天骄 1郑锡涛 1范献银 1郑晓霞2

作者信息

  • 1. 西北工业大学航空学院,西安710072
  • 2. 沈阳发动机设计研究所,沈阳110015
  • 折叠

摘要

Abstract

Damage of composite laminates due to low-velocity impact depends on number of factors. The simulation of composite laminates damage is carried out with ABAQUS software. Several influence factors are analyzed in order to foresee the damage resistance of composite laminates in the early stage with the method which regards damage area as the single-variable parameter. Delamination is one of leading damage forms of laminates. Based on damage mechanics, fracture mechanics and cohesive theory, cohesive unites are constituted in this paper to simulate delamination accurately. The point of inflexion is a central characterization of damage resistance. Based on the experiments and finite element model, damage resistances of different laminates are determined by contrasting diverse inflexion value which can be calculated on impact force-time curves. The rationality of the model has been confirmed by the low-velocity impact test.

关键词

冲击损伤/影响因素/材料体系/冲头/铺层序列

Key words

impact damage/ influence factor/ material system/ impactor/ lay-up sequence

分类

通用工业技术

引用本文复制引用

屈天骄,郑锡涛,范献银,郑晓霞..复合材料层合板低速冲击损伤影响因素分析[J].航空材料学报,2011,31(6):81-86,6.

基金项目

国家自然科学基金(10872167) (10872167)

航空材料学报

OA北大核心CSCDCSTPCD

1005-5053

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