Guan Miao, Shen Songhua, Wang Yong, et al. Aeronautical static inverter based on repetitive control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1223-1227. (in Chinese)
Citation: WANG Xiao-jun, TONG Zhong-hua, JIANG Chi-pinget al. Prediction of Axial Longitudinal Shear Modulus of Multiphase Fiber Composites[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(3): 335-338. (in Chinese)

Prediction of Axial Longitudinal Shear Modulus of Multiphase Fiber Composites

  • Received Date: 12 Oct 2000
  • Publish Date: 31 Mar 2002
  • A generalized self-consistent model to predict the effective longitudinal shear modulus of multiphase fiber composites was developed, by considering the effect of fiber section shape. In the model, combined confocal elliptical cylinder unit cells are embedded in an infinite homogenization composite. By using conformal mapping technique and Laurent series expansion, a close form solution was obtained. Further a group of algebraic equations to predict effective longitudinal shear modulus of multiphase fiber composites were obtained by virtue of the averaged stress-strain theorem. When the shear moduli of all fibers are same, the above equations can be reduced to those for single phase fiber reinforced composites. The validity of the proposed model was verified by comparing present theoretical predictions with available experimental results.

     

  • [1]张佐光,张晓宏,仲伟虹,等. 多相混杂纤维复合材料拉伸行为分析 .张志民.第九届全国复合材料学术会议论文集:下册 .北京:世界图书出版公司,1996.410~416. [2]王震鸣,范赋群. 复合材料及其结构力学进展(第二册)[M].广州:华南理工大学出版社,1991. [3]许凤和.高分子材料力学实验[M].北京:科学出版社,1988. [4]Christense R M. Effective properties of composite materials containing voids . Proceedings of the Royal Society of London A440 . 1993.461~473. [5]Jiang C P, Cheung Y K. A fiber/matrix/composite model with a combined confocal elliptical cylinder unit cell for predicting the effective longitudinal shear modulus[J]. Int J Solids Structures,1998,35(30):3977~3987. [6]Whitney J M, Riley M B. Elastic properties of fiber reinforced composite materials[J]. AIAA J,1966,4(9):1537~1542. [7]Huang Y, Hu K X. A generalize self-consistent mechanics method for solids containing elliptical inclusions[J]. ASME Journal of Applied Mechanics,1995,62:566~572, [8]Мусхелишвили著.数学弹性力学的几个基本问题[M]. 赵惠元译.北京:科学出版社,1958.
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