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Fatigue life prediction and experiment research for composite laminates with circular hole 被引量:1

Fatigue life prediction and experiment research for composite laminates with circular hole
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摘要 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. 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.
出处 《Journal of Central South University of Technology》 2004年第1期19-22,共4页 中南工业大学学报(英文版)
基金 Project ( 2 4.8.1.2 6)supportedbyPre researchProjectoftheAeronauticalScienceFoundationofChina
关键词 碾压 合成材料 静力学 金属材料 composite material fatigue Whitney-Nuismer criterion laminate with a hole
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  • 1E. K. Gamstedt,S. ?stlund.Fatigue Propagation of Fibre-Bridged Cracks in Unidirectional Polymer-Matrix Composites[J].Applied Composite Materials.2001(6)
  • 2NOBUO OTANI,DONG-YEUL SONG.Fatigue life prediction of composites under two-stage loading[J].Journal of Materials Science.1997(3)
  • 3.Tensile tensilefatiguetestmethodfortheFRCmaterial[].HB.
  • 4.Thestatictestingmethodforthefiberrein forcedplastics[].GB.
  • 5Chen,Hua-hui,Deng,Hai-jing,Li,Ming. Modern Composite Material . 1998
  • 6Zhang,Yao,Li,You-qin. The Aviation Composite Material Technology Achievements: The Development of Our Country Aviation Composite Material Technology . 1998
  • 7Gamsted E K.Fatigue propagation of fibre-bridged cracks in unidirectional polymer-matrix composites[].Applied Composite Materials.2001
  • 8Hahn H T.Fatigue life prediction and failure mechanisms of composite materials[].Advances in Computational Mathematics.1992
  • 9Whitwoth H A.Evaluation of the residual strength degradation in composite laminates under loading[].Composite Structures.2001
  • 10Li,Shun-lin. Composite Materials Handbook . 1989

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