缝合复合材料层板三维纤维弯曲模型及压缩强度预报

李晨, 许希武

李晨, 许希武. 缝合复合材料层板三维纤维弯曲模型及压缩强度预报[J]. 复合材料学报, 2006, 23(6): 179-185.
引用本文: 李晨, 许希武. 缝合复合材料层板三维纤维弯曲模型及压缩强度预报[J]. 复合材料学报, 2006, 23(6): 179-185.
LI Chen, XU Xi-wu. 3D f iber waviness model and prediction of compressive strength of stitched laminates[J]. Acta Materiae Compositae Sinica, 2006, 23(6): 179-185.
Citation: LI Chen, XU Xi-wu. 3D f iber waviness model and prediction of compressive strength of stitched laminates[J]. Acta Materiae Compositae Sinica, 2006, 23(6): 179-185.

缝合复合材料层板三维纤维弯曲模型及压缩强度预报

基金项目: 航空基金(05G52054)
详细信息
    通讯作者:

    许希武, 研究员, 从事复合材料结构力学、飞行器结构完成性评定技术及计算力学领域的科研工作 E-mail : xwxu @nuaa. edu. cn

  • 中图分类号: TB332

3D f iber waviness model and prediction of compressive strength of stitched laminates

  • 摘要: 提出了三维纤维弯曲模型, 基于有限元法和周期性边界条件建立了缝合层板压缩强度分析方法, 采用桥联模型和最大应力判据分析损伤扩展并获得压缩强度, 预报结果与试验吻合较好。详细探讨了缝合参数对层合板压缩强度的影响规律, 结果表明: 缝合方向与表面纤维方向一致时, 较小的缝合针距和行距、较大的缝合线半径对压缩强度较为有利; 缝合方向与表面纤维方向垂直时, 较小的缝合针距和缝合线半径、较大的缝合行距对压缩强度较为有利。
    Abstract: A 3D fiber waviness model was presented. Based on the finite element method and periodic boundaryconditions , a method to analyze the compressive st rength of stitched laminates was established , which adopted abridging model and maximum st ress criteria to predict the development of damage and obtain the compressivest rength. The predicted result s are in good agreement with the test data. The effects of stitching parameters on thecompressive st rength of stitched laminates are discussed in detail. The results indicate that when stitching along thefiber on the surface of laminates , smaller stitch space and step and larger stitch radius result in higher compressivest rength. However , when stitching perpendicular to the fiber on the surface , smaller stitch space and radius andlarger stitch step result in higher compressive st rength.
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出版历程
  • 收稿日期:  2006-01-08
  • 修回日期:  2006-05-07
  • 刊出日期:  2006-12-14

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