Fatigue life prediction and experiment research for composite laminates with circular hole

Hong-yu Qi , Wei-dong Wen , Lian-wen Xun

Journal of Central South University ›› 2004, Vol. 11 ›› Issue (1) : 19 -22.

PDF
Journal of Central South University ›› 2004, Vol. 11 ›› Issue (1) : 19 -22. DOI: 10.1007/s11771-004-0004-7
Article

Fatigue life prediction and experiment research for composite laminates with circular hole

Author information +
History +
PDF

Abstract

Based on the fatigue prediction model of exponential function and Whitney-Nuismer(WN) criterion of static strength for the composite material laminate with a circular hole, the stress correct factor (β) was put forward and a new fatigue prediction model for composite material laminate was set up. T300/KH304, which is recently studied and is a high capability composite material, was used as the raw material. In order to gain the factor β, the fatigue experiments of the laminates with holes in different diameters and the same ratio of width to diameter were conducted. The fatigue analysis and tests of the laminates with a hole 5 mm in diameter are carried out at different stress levels, and the results meet the engineering requirement. The simple, prompt and practical method is provided for the prediction of S-N curve of composite laminate with a circular hole.

Keywords

composite material / fatigue / Whitney-Nuismer criterion / laminate with a hole

Cite this article

Download citation ▾
Hong-yu Qi, Wei-dong Wen, Lian-wen Xun. Fatigue life prediction and experiment research for composite laminates with circular hole. Journal of Central South University, 2004, 11(1): 19-22 DOI:10.1007/s11771-004-0004-7

登录浏览全文

4963

注册一个新账户 忘记密码

References

[1]

ChenHua-hui, DengHai-jing, LiMing, et al.Modern Composite Material [M], 1998, Beijing, China Logistics Publishing House(in Chinese)

[2]

ZhangYao, LiYou-qinThe Aviation Composite Material Technology Achievements: The Development of Our Country Aviation Composite Material Technology [M], 1998, Beijing, Aviation Industry Press(in Chinese)

[3]

GamstedE K. Fatigue propagation of fibre-bridged cracks in unidirectional polymer-matrix composites [J]. Applied Composite Materials, 2001, 8(3): 385-410

[4]

HahnH T. Fatigue life prediction and failure mechanisms of composite materials [J]. Advanced Comp Mat, 1992, 2(1): 29-50

[5]

WhitwothH A. Evaluation of the residual strength degradation in composite laminates under loading [J]. Composite Structures, 2001, 48(2): 261-264

[6]

ZhaiHong-jun, YaoWei-xing. Recent research of stiffness degradation for FRC [J]. Advances in Mechanics, 2002, 32(1): 69-80(in Chinese)

[7]

NobuoO M. Fatigue life prediction of composites under two-stage loading [J]. J Materials Science, 1997, 32(4): 755-760

[8]

LiShun-linComposite Materials Handbook [M], 1989, Beijing, Aviation Industry Press(in Chinese)

[9]

WuWen-fang. A study of fatigue damage and fatigue life of composite laminates [J]. J Comp Mat, 1996, 30(1): 123-137

[10]

HaoYongDamage Research of Composite Materials Laminate with Circle Hole [D], 1999, Nanjing, Nanjing University of Aeronautics and Astronautics(in Chinese)

[11]

HB5440-89. Tensile-tensile fatigue test method for the FRC material [S]. (in Chinese)

[12]

QiHong-yuStudy on Buckling and Fatigue Life of Composite and Aeroengine Composite Case [D], 2001, Nanjing, Nanjing University of Aeronautics and Astronautics(in Chinese)

[13]

GB3354-82. The static testing method for the fiber reinforced plastics [S]. (in Chinese)

AI Summary AI Mindmap
PDF

137

Accesses

0

Citation

Detail

Sections
Recommended

AI思维导图

/