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考虑分层损伤的完全抛物线剪切滞后模型 被引量:2

A COMPLETE PARABOLIC SHEAR-LAG MODEL CONTAINING DELAMINATION DAMAGE
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摘要 横向基体开裂和分层损伤是正交层板复合材料的主要损伤类型.与现有完全抛物线剪切滞后分析模型不同,本文提出了包含横向开裂裂尖引起分层损伤的完全抛物线模型.依此模型计算了材料的刚度衰减,并与不包含分层的完全抛物线、不完全抛物线等剪切滞后分析模型预测结果作了计算比较.结果表明,在应力较高的情况下,本文提出的分析模型所得的预测结果与实验值符合得最好. A complete parabolic shear-lag model containing delamination damage induced by transverse cracks was proposed and applied to predict the stiffness reduction by transverse cracking in cross laminated composite materials. The relation of stress and transverse crack density was also studied. The predictions from the incomplete parabolic shear-lag analysis model, the complete parabolic shear-lag analysis model and the analysis model proposed in this paper have been compared. Results show that the Young's modulus reduction values obtained by our analysis model are better agreement with the experimental ones than other models.
出处 《金属学报》 SCIE EI CAS CSCD 北大核心 2001年第10期1027-1030,共4页 Acta Metallurgica Sinica
关键词 纤维增强层板复合材料 分层损伤 完全抛物线剪滞模型 fiber-reinforced composite laminate delaminate damage parabolic shear-lag model
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参考文献1

  • 1Lee J W,Compos Sci Technol,1990年,24卷,1225页

同被引文献10

  • 1佟丽莉,陈辉,孟松鹤,杜善义.纤维缠绕复合材料壳体刚度衰减模型数值模拟[J].复合材料学报,2004,21(5):159-164. 被引量:15
  • 2佟丽莉,梁军,杜善义.复合材料层板损伤后刚度衰退的实验研究[J].实验力学,2005,20(2):259-264. 被引量:4
  • 3Reifsnider K L.Some Fundamental Aspects of the Fatigue and Fracture Response of Composite Materials[C].//Proceedings of 14th Annual Meeting of Soc.Eng.Sci,Bethlehem,USA,1977:373-384
  • 4Garret K W,Bailey J E.Multiple Transverse Fracture in 90° Cross-ply Laminates of a Glass Fibre-reinforced Polyester[J].J Mater Sic 1977,12:157-168
  • 5Parvizi A,Garrett K W,Bailey J E.Constrained Cracking in Glass Fiber-reinforced Epoxy Cross-ply Laminates[J].J Mater Sci,1978,13:195-201
  • 6Highsmith A L,Reifsnider K L.Stiffness Reduction Mechanisms in Composite Laminates[C].// Damage in Composite Materials ASTM STP 775 (Ed.K.L.Reifsnider),American Society for Testing and Materials Philadelphia,PA.1982:103-117
  • 7Ogin S L,Smity P A,Beauinont P W R.Matrix Cracking and Stiffness Reduction During the Fatigue of a (0/90)s GFRP laminate[J].Compos Sci Technol,1985,22:23-31.
  • 8Manders P W,Chou T W,Jones F R,et al.Statistical Analysis of Multiple Fracture in 0°/90°/0°galss Fibre/epoxy Resin Laminates[J].J Mater Sci 1983,18:2 876-2 889
  • 9Berthelot J M,Leblond P,Mahi A E I,et al.Transverse Cracking of Cross-ply Laminates:part1 Analysis[J].Composites Part A,1996,27A:989-1 001
  • 10Shinji Ogihara, Nobuo Takeda. Interaction between transverse cracks and delamination during damage progress in CFRP cross-ply laminates [J]. Composites Science and Technology (S0266-3538), 1995, 54(5): 396-404.

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